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Title: Stamp Act = Debates sobre acto ... da America.
Abstract/Description: Manuscript in an unidentified hand, undated, concerning the Parliamentary debates on the repeal of the Stamp Act of Great Britain. Parallel text in English and Spanish on opposite pages. Caption title of English text may be cutoff due to trimming. Fourth word of caption title of Spanish text mostly lost due to trimming. First and last pages blank. Bears watermark of a Fleur-de-lis and the letters "BDXXG" within. Has catchwords, side notes, tie-holes.
Date Issued: 1765 - 1766
PURL: http://purl.flvc.org/fau/fd/fauwdlb1f10
Format: E-book

Title: An oration, pronounced at Sutton, Massachusetts, July 5th, 1813 : in commemoration of American independence.
Creator: Bangs, Edward D. (Edward Dillingham) 1790-1838
Abstract/Description: by Edward D. Bangs, Esq., published by request. In commemoration of American independence. Includes bibliographical references. FAU copy appears to have been trimmed to 21 cm; title page inscription by E.D. Bangs cut off from trimming.
PURL: http://purl.flvc.org/fau/fd/fauwsb9f22
Subject Headings: Fourth of July addresses -- 1813, Fourth of July celebrations -- Massachusetts -- Sutton, Fourth of July orations -- 19th century, Speeches, addresses, etc., American, Speeches, addresses, etc., American -- 19th century, United States -- History -- War of 1812, United States -- Politics and government -- 1812-1815
Format: E-book

Title: An oration, pronounced July 4, 1800, at the request of the inhabitants of the town of Boston : in commemoration of the anniversary of American independence.
Creator: Hall, Joseph 1761-1848, Manning & Loring
Abstract/Description: Published by request of the town. Signatures: [A]⁴ B-C⁴. Title vignette. Engraved head-piece. Includes bibliographical references. FAU Libraries' copy appears to have been trimmed to 21 cm; title page inscription by J. Hall cut off from trimming.
PURL: http://purl.flvc.org/fau/fd/fauwsb8f17
Subject Headings: Fourth of July addresses -- 1800, Fourth of July celebrations -- Massachusetts -- Boston -- Early works to 1800, Fourth of July orations -- 18th century -- Early works to 1800, Massachusetts -- Boston, Speeches, addresses, etc., American -- 18th century, United States -- History -- 1797-1801 -- Sources -- Early works to 1800, United States -- Politics and government -- 1783-1789 -- Early works to 1800, United States -- Politics and government -- 1797-1801 -- Early works to 1800
Format: E-book

Title: Dynamic stall and three-dimensional wake effects on isolated rotor trim and stability with experimental correlation and parallel fast-Floquet analysis.
Creator: Subramanian, Shanmugasundaram., Florida Atlantic University, Gaonkar, Gopal H., College of Engineering and Computer Science, Department of Ocean and Mechanical Engineering
Abstract/Description: Hingeless rotors are susceptible to instabilities of the lead-lag or lag modes, which are at best weakly damped. The lag mode derives its damping primarily from the complex rotor flow field that is driven by interdependent dynamics of airfoil stall and rotor downwash or wake. Therefore, lag-damping prediction requires an aerodynamic representation that adequately accounts for quasisteady stall, dynamic stall and three-dimensional dynamic wake. Accordingly, this dissertation investigates these...
Show moreHingeless rotors are susceptible to instabilities of the lead-lag or lag modes, which are at best weakly damped. The lag mode derives its damping primarily from the complex rotor flow field that is driven by interdependent dynamics of airfoil stall and rotor downwash or wake. Therefore, lag-damping prediction requires an aerodynamic representation that adequately accounts for quasisteady stall, dynamic stall and three-dimensional dynamic wake. Accordingly, this dissertation investigates these stall and wake effects on lag damping and demonstrates the strengths and weaknesses of the aerodynamic representation with a comprehensive experimental correlation. The database refers to a three-bladed rotor operated untrimmed and to a fourbladed rotor operated trimmed; for both rotors, the blade collective pitch and shaft tilt angles are set prior to each test run. The untrimmed rotor is tested with advance-ratios as high as 0.55 and shaft angles as high as 20°, and it has intentionally builtin structural simplicity: torsionally stiff blades and no swash plate. The trimmed rotor has torsionally soft blades; it is trimmed in the sense that the longitudinal and lateral cyclic pitch controls are adjusted through a swash plate to minimize l/rev root flap moment. Therefore, for the untrimmed rotor, the database refers to lagdamping levels, and for the trimmed rotor, it refers to lag-damping levels as well as to trim results of lateral and longitudinal cyclic pitch controls and steady root flap moments. The dynamic stall representation is based on the ONERA models of lift, drag and pitching moment, and the unsteady wake is described by a finite-state three-dimensional wake model. The root-flexure-blade assembly of the untrimmed rotor is represented by a root-restrained rigid flap-lag model as well as by an elastic flap-lag-torsion model. Similarly, the trimmed rotor is represented by an elastic flaplag- torsion model. The predictions are from three aerodynamic theories ranging from a quasisteady stall theory to a fairly comprehensive dynamic stall and wake theory. This dissertation also addresses the computational aspects of lag-damping predictions by parallel F!oquct analysis based on classical and fast Floquet theories. In a typical trimmed flight, the Floquet analysis comprises (i) trim or equilibrium analysis, (ii) generation of the Floquet transition matrix (FTM) about the trim position, and (iii) eigenanalysis of the FTM. The trim analysis involves the computations of the unknown control inputs that satisfy flight conditions of required thrust and force-moment equilibrium as well as the initial conditions that guarantee periodic forced response. The shooting method is increasingly used for the trim analysis since it generates the FTM as a byproduct and is not sensitive to damping levels. The QR method is used almost exclusively for the FTM eigenanalysis. Presently, the Floquet analysis with shooting and QR methods is widely used for small-order systems (number of states or order M < 100). However, it has been found to be practical neither for design nor for comprehensive-analysis models that lead to large systems (A11 > 100); the run time on a conventional sequential computer is simply prohibitive. Nevertheless, all three parts of Floquet analysis can be algorithmically structured such that they lend themselves well to parallelism or concurrent computations. Furthermore, the conventional Floquet analysis requires integrations of equations of motion through one complete period T; and the bulk of the run time is for repeated integrations over one period. However, for rotors with Q identical blades, it is computationally advantageous to use the fast Floquet analysis, which requires integration through a period T/Q. Accordingly, this dissertation develops parallel algorithms for classical Floquet analysis with classical shooting and for the fast Floquet analysis with fast shooting; in each case the FTM eigenanalysis is baseJ on a parallel QR tibrary routine. The computational reliability· of the sequential anJ parallel Floquet analyses is quantified by (i) the condition number of the converged Jacobian matrix in Newton iteration of trim analysis, (ii) the condition numbers of the FTM eigenvalues of interest, and (iii) the corresponding residual errors of the eigenpairs (eigenvalue and the corresponding eigenYector). These algorithms are applied to study (i) linear flap stability with dynamic wake, (ii) nonlinear flaplag stability with dynamic wake under propulsive- or flight-trim conditions. and (iii) noniinear fiap-iag stabiiity with dynamic staii and wake under flight trim conditions. The parallel and sequential algorithms are compared with respect to computational reliability, saving in run time and growth of run time with increasing system order. Other parallel performance metrics such as speedup, efficiency, and sequential and parallel fractions are included as well. The computational reliability figures of the four algorithms - classical and fast-Floquet analyses each in sequential and parallel modes - are comparable. The fast-Floquet analysis brings in nearly Q-fold reduction in run time in both the sequential and parallel modes; that is, its advantages apply equally to both the modes. 'While the run times for the classical- and fast-Floquet analyses in sequential mode grow in between quadratically and cubically with the system order, the corresponding run times in parallel mode are far shorter and more importantly remain nearly constant. These results offer considerable promise in making large-scale Floquet analysis practical for rotorcrafts with identical as well as with dissimilar blades.
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Date Issued: 1996
PURL: http://purl.flvc.org/fcla/dt/12462
Subject Headings: Rotors (Helicopters), Stalling (Aerodynamics), Drag (Aerodynamics), Wakes (Aerodynamics), Floquet theory
Format: Document (PDF)

Title: Trim analysis by shooting and finite elements and Floquet eigenanalysis by QR and subspace iterations in helicopter dynamics.
Creator: Achar, Nagari Shriranga., Florida Atlantic University, Gaonkar, Gopal H., College of Engineering and Computer Science, Department of Ocean and Mechanical Engineering
Abstract/Description: The trim analysis for the initial state and control inputs that satisfy response periodicity and flight conditions, and the Floquet eigenanalysis for a few largest eigenvalues of the Floquet transition matrix (FTM) are investigated. In the trim analysis, the convergence of Newton iteration is investigated in computing the periodic initial state and control inputs sequentially and in parallel. The trim analysis uses the shooting method and two h-versions of temporal finite element methods, one...
Show moreThe trim analysis for the initial state and control inputs that satisfy response periodicity and flight conditions, and the Floquet eigenanalysis for a few largest eigenvalues of the Floquet transition matrix (FTM) are investigated. In the trim analysis, the convergence of Newton iteration is investigated in computing the periodic initial state and control inputs sequentially and in parallel. The trim analysis uses the shooting method and two h-versions of temporal finite element methods, one based on displacement formulation and the other on mixed formulation of displacements and momenta. In each method, both the sequential and in-parallel schemes are used, and the resulting nonlinear equations are solved by damped Newton iteration with an optimally selected damping parameter. The reliability of damped Newton iteration, including earlier-observed divergence problems, is quantified by the maximum condition number of the Jacobian matrices of the iterative scheme. For illustrative purposes, rigid flap-lag and flap-lag-torsion models based on quasisteady aerodynamics are selected. Demanding trim analysis conditions are included by considering advance ratios or dimensionless flight speeds twice as high as those of current helicopters. Concerning the Floquet eigenanalysis, the feasibility of using the Arnoldi-Saad method, one of the emerging subspace iteration methods, is explored as an alternative to the currently used QR method, which is not economical for partial eigenanalysis. The reliability of the Arnoldi-Saad method is quantified by the eigenvalue condition numbers and the residual errors of the eigenpairs. In the three trim analysis methods, while the optimally selected damping parameter provides almost global convergence, the in-parallel scheme requires much less machine time than the conventional sequential scheme; both schemes have comparable reliability of the Newton iteration without and with damping. The Arnoldi-Saad method takes much less machine time than the QR method with comparable reliability.
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Date Issued: 1992
PURL: http://purl.flvc.org/fcla/dt/12297
Subject Headings: Helicopters--Dynamics, Helicopters--Handling characteristics, Stability of helicopters--Mathematical models
Format: Document (PDF)

Title: Dynamic stall and three-dimensional wake effects on trim, stability and loads of hingeless rotors with fast Floquet theory.
Creator: Chunduru, Srinivas Jaya., Florida Atlantic University, Gaonkar, Gopal H., College of Engineering and Computer Science, Department of Ocean and Mechanical Engineering
Abstract/Description: This dissertation investigates the effects of dynamic stall and three-dimensional wake on isolated-rotor trim, stability and loads. Trim analysis of predicting the pilot's control inputs and the corresponding periodic responses is based on periodic shooting with the fast Floquet theory and damped Newton iteration. Stability analysis, also based on the fast Floquet theory, predicts damping levels and frequencies. Loads analysis uses a force-integration approach to predict the rotating-blade...
Show moreThis dissertation investigates the effects of dynamic stall and three-dimensional wake on isolated-rotor trim, stability and loads. Trim analysis of predicting the pilot's control inputs and the corresponding periodic responses is based on periodic shooting with the fast Floquet theory and damped Newton iteration. Stability analysis, also based on the fast Floquet theory, predicts damping levels and frequencies. Loads analysis uses a force-integration approach to predict the rotating-blade root shears and moments as well as the hub forces and moments. The blades have flap bending, lag bending and torsion degrees of freedom. Dynamic stall is represented by the ONERA stall models of lift, drag and pitching moment, and the unsteady, nonuniform downwash is represented by a three-dimensional, finite-state wake model. Throughout, full blade-stall-wake dynamics is used in that all states are included from trim to stability to loads predictions. Moreover, these predictions are based on four aerodynamic theories--quasisteady linear theory, quasisteady stall theory, dynamic stall theory and dynamic stall and wake theory--and cover a broad range of system parameters such as thrust level, advance ratio, number of blades and blade torsional frequency. The investigation is conducted in three phases. In phase one, the elastic flap-lag-torsion equations are coupled with a finite-state wake model and with linear quasisteady airfoil aerodynamics. The investigation presents convergence characteristics of trim and stability with respect to the number of spatial azimuthal harmonics and radial shape functions in the wake representation. It includes a comprehensive parametric study over a broad range of system parameters. The investigation also includes correlation with the measured lag-damping data of a three-bladed isolated rotor operated untrimmed. In the correlation, three structural models of the root-flexure-blade assembly are used to demonstrate the strengths and the weaknesses of lag-damping predictions. Phase two includes dynamic stall in addition to three-dimensional wake to generate trim and stability results over a comprehensive range of system parameters. It addresses the degree of sophistication necessary in blade discretization and wake representation under dynamically stalled conditions. The convergence and parametric studies isolate the effects of wake, quasisteady stall and dynamic stall on trim and stability. Finally, phase three predicts the rotating blade loads and nonrotating hub loads; the predictions are based on the blade, wake and stall models used in the preceding trim and stability investigations. Although an accurate evaluation of loads requires a more refined blade description, the results isolate and demonstrate the principal dynamic stall and wake effects on the loads.
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Date Issued: 1995
PURL: http://purl.flvc.org/fcla/dt/12426
Subject Headings: Floquet theory, Helicopters, Rotors (Helicopters), Vibration (Aeronautics)
Format: Document (PDF)

Title: Helicopter stability during aggressive maneuvers.
Creator: Mohan, Ranjith., College of Engineering and Computer Science, Department of Ocean and Mechanical Engineering
Abstract/Description: The dissertation investigates helicopter trim and stability during level bank-angle and diving bank-angle turns. The level turn is moderate in that sufficient power is available to maintain level maneuver, and the diving turn is severe where the power deficit is overcome by the kinetic energy of descent. The investigation basically represents design conditions where the peak loading goes well beyond the steady thrust limit and the rotor experiences appreciable stall. The major objectives are:...
Show moreThe dissertation investigates helicopter trim and stability during level bank-angle and diving bank-angle turns. The level turn is moderate in that sufficient power is available to maintain level maneuver, and the diving turn is severe where the power deficit is overcome by the kinetic energy of descent. The investigation basically represents design conditions where the peak loading goes well beyond the steady thrust limit and the rotor experiences appreciable stall. The major objectives are: 1) to assess the sensitivity of the trim and stability predictions to the approximations in modeling stall, 2) to correlate the trim predictions with the UH-60A flight test data, and 3) to demonstrate the feasibility of routinely using the exact fast-Floquet periodic eigenvector method for mode identification in the stability analysis. The UH-60A modeling and analysis are performed using the comprehensive code RCAS (Army's Rotorcraft Comprehensive Analysis System). The trim and damping predictions are based on quasisteady stall, ONERA-Edlin vi (Equations Differentielles Lineaires) and Leishman-Beddoes dynamic stall models. From the correlation with the test data, the strengths and weaknesses of the trim predictions are presented.
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Date Issued: 2012
PURL: http://purl.flvc.org/FAU/3342237
Subject Headings: Helicopters, Aerodynamics, Helicopters, Control systems, Rotors (Helicopters), Aerodynamics, Stability of helicopters, Vibration (Aeronautics), Damping
Format: Document (PDF)

Title: Parallel-computing concepts and methods toward large-scale floquet analysis of helicopter trim and stability.
Creator: Nakadi, Rajesh Mohan., Florida Atlantic University, Gaonkar, Gopal H., College of Engineering and Computer Science, Department of Ocean and Mechanical Engineering
Abstract/Description: The rotorcraft trim solution involves a search for control inputs for required flight conditions as well as for corresponding initial conditions for periodic response or orbit. The control inputs are specified indirectly to satisfy flight conditions of prescribed thrust levels, rolling and pitching moments etc. In addition to the nonlinearity of the equations of motion and control inputs, the control inputs appear not only in damping and stiffness matrices but also in the forcing-function or...
Show moreThe rotorcraft trim solution involves a search for control inputs for required flight conditions as well as for corresponding initial conditions for periodic response or orbit. The control inputs are specified indirectly to satisfy flight conditions of prescribed thrust levels, rolling and pitching moments etc. In addition to the nonlinearity of the equations of motion and control inputs, the control inputs appear not only in damping and stiffness matrices but also in the forcing-function or input matrix; they must be found concomitantly with the periodic response from external constraints on the flight conditions. The Floquet Transition Matrix (FTM) is generated for perturbations about that periodic response; usually, a byproduct of the trim analysis. The damping levels or stability margins are computed from an eigenanalysis of the FTM. The Floquet analysis comprises the trim analysis and eigenanalysis and is routinely used for small order systems (order N < 100). However, it is practical for neither design applications nor comprehensive analysis models that lead to large systems (N > 100); the execution time on a sequential computer is prohibitive. The trim analysis takes the bulk of this execution time. Accordingly, this thesis develops concepts and methods of parallelism toward Floquet analysis of large systems with computational reliability comparable to that of sequential computations. A parallel shooting scheme with damped Newton iteration is developed for the trim analysis. The scheme uses parallel algorithms of Runge-Kutta integration and linear equations solution. A parallel QR algorithm is used for the eigenanalysis of the FTM. Additional parallelism in each iteration cycle is achieved by concurrent operations such as perturbations of initial conditions and control inputs, follow-up integrations and formations of the columns of the Jacobian matrix. These parallel shooting and eigenanalysis schemes are applied to the nonlinear flap-lag stability with a three-dimensional dynamic wake (N ~ 150). The stability also is investigated by widely used sequential schemes of shooting with damped Newton iteration and QR eigenanalysis. The computational reliability is quantified by the maximum condition number of the Jacobian matrices in the Newton iteration, the eigenvalue condition numbers and the residual errors of the eigenpairs. The saving in computer time is quantified by the speedup, which is the ratio of the execution times of Floquet analysis by sequential and parallel schemes. The work is carried out on massively parallel MasPar MP-1, a distributed-memory, single-instruction multiple-data or SIMD computer. A major finding is that with increasing system order, while the parallel execution time remains nearly constant, the sequential execution time increases nearly cubically with N. Thus, parallelism promises to make large-scale Floquet analysis practical.
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Date Issued: 1994
PURL: http://purl.flvc.org/fcla/dt/15085
Subject Headings: Floquet theory, Helicopters--Control systems, Rotors (Helicopters), Parallel processing (Electronic computers)
Format: Document (PDF)

Title: An address delivered before the New England Society of Philadelphia; at its semiannual meeting in May, 1824.
Creator: Bond, Henry 1790-1859, New England Society of Philadelphia
Abstract/Description: By Henry Bond, M.D.
PURL: http://purl.flvc.org/fau/fd/fauwsb9f36
Subject Headings: Massachusetts -- History -- Colonial period, ca. 1600-1775, New England -- History -- Colonial period, ca. 1600-1775, Pilgrims (New Plymouth Colony), Speeches, addresses, etc., American -- 19th century, United States -- History -- Revolution, 1775-1783
Format: E-book

Title: The throne of iniquity, or, Sustaining evil by law : a discourse in behalf of a law prohibiting the traffic in intoxicating drinks delivered in the First Presbyterian Church, Philadelphia, Feb. 1, 1852, and in the Presbyterian Church, Harrisburg, Feb. 29, 1852.
Creator: Barnes, Albert 1798-1870, Theo. Fenn & Co.
Abstract/Description: Sustaining evil by law. First Presbyterian Church (Philadelphia, Pa.). Presbyterian Church (Harrisburg, Pa.) "Published by request." Printed in two columns. FAU copy imperfect: pages trimmed rough and too closely along fore edge with some loss of text; trimmed to 22 cm.
PURL: http://purl.flvc.org/fau/fd/fauwsb16f13
Subject Headings: Alcoholic beverages -- Sermons, Liquor laws -- United States -- States -- Sermons, Philadelphia (Pa.) -- Social conditions -- Sermons, Sermons, American -- 19th century, Drinking of alcoholic beverages -- Moral and ethical aspects -- Sermons, Maine -- Laws, etc, Bible -- Psalms, XCIV, 20 -- Sermons, Prohibition -- United States -- Sermons, American Temperance Union, Temperance -- United States -- Sermons
Format: E-book

Title: A discourse preached December 15th, 1774 : being the day recommended by the Provincial Congress; and afterwards at the Boston Lecture.
Creator: Gordon, William 1728-1807, Leverett, Thomas 1730-1778
Abstract/Description: By William Gordon. Pastor of the Third Church in Roxbury. [Eleven lines of quotations]. The second edition. Half title: Mr. Gordon's Thanksgiving discourse. Running title: Thanksgiving discourse.Signatures: [A]⁴ B-D⁴. Includes bibliographical references. FAU Libraries' have two copies that appear to have been trimmed. First copy rebound in contemporary binding with marbled paper covers and gold stamping on spine (very closely trimmed, affecting text at bottom edges).
PURL: http://purl.flvc.org/fau/fd/fauwsb3f10
Subject Headings: Bible -- Lamentations, III, 22 -- Sermons -- Early works to 1800, Boston (Mass.) -- History -- Colonial period, ca. 1600-1775 -- Sources -- Early works to 1800, Thanksgiving Day addresses -- Sermons -- Early works to 1800, Thanksgiving sermons -- 1774 December 15, Liberty -- Sermons -- Early works to 1800, Sermons, American -- 18th century, United States -- History -- Revolution, 1775-1783 -- Causes -- Sources -- Early works to 1800
Format: E-book

Title: The encroachments and exactions of slavery : speech of the Hon. Horatio J. Stow.
Creator: Stow, Horatio J. 1859, Laflin, Addison Henry 1823-1878
Abstract/Description: Speech of the Honorable Horatio J. Stow, of Niagara County. Notes: Caption title. Text printed in two columns. FAU copy pages trimmed too closely along bottom edge with some loss of text on page 10; trimmed to 22 cm. Page [1] has ink stamp: "A.H. Laflin, Senator, 20th District."
PURL: http://purl.flvc.org/fau/fd/fauwsb18f18
Subject Headings: Congressional addresses -- United States -- 19th century, Slavery -- Political aspects -- United States -- History -- 19th century -- Sources, Slavery -- United States -- Extension to the territories -- Speeches in Congress, Slavery -- United States -- Speeches in Congress, Speeches, addresses, etc., American -- 19th century, United States -- Politics and government -- 1857-1861
Format: E-book

Title: A discourse delivered at Wethersfield, December 11th, 1783 : being a day of public thanksgiving, throughout the United States of America.
Creator: Marsh, John 1742-1821, First Church of Christ (Wethersfield, Conn.)
Abstract/Description: By John Marsh, A.M., pastor of the First church and society in Wethersfield ; published at the desire and expence of said society. Half-title: Mr. Marsh's discourse on the public thanksgiving, MDCCLXXXIII. Signatures: [A]⁴ B-C⁴ (C4 blank). FAU Libraries' have two copies. First copy appears to have been trimmed to 23 cm.; side stiched with brown cord. Second copy trimmed to 20 cm.
PURL: http://purl.flvc.org/fau/fd/fauwsb7f7
Subject Headings: American Revolution (1775-1783), Bible -- Psalms, CXLVII, 12-14 -- Sermons -- Early works to 1800, Connecticut -- History -- Revolution, 1775-1783 -- Sources -- Early works to 1800, Gratitude -- Religious aspects -- Sermons -- Early works to 1800, Sermons, American -- 18th century, Thanksgiving Day addresses -- Sermons -- Early works to 1800, Thanksgiving sermons -- 1783 Dec. 11, United States -- History -- Revolution, 1775-1783 -- Peace -- Early works to 1800
Format: E-book

Title: A discourse, delivered at Lancaster, on the day of annual thanksgiving. Nov. 27, 1828.
Creator: Thayer, Nathaniel 1769-1840, Carter, Andrews & Co.
Abstract/Description: By Nathaniel Thayer, D.D. Minister of Lancaster. FAU copy edges trimmed to 17 cm.
PURL: http://purl.flvc.org/fau/fd/fauwsb10f17
Subject Headings: Thanksgiving Day addresses -- Massachusetts -- Lancaster -- 1828, Bible -- Psalms, C, 4 -- Sermons, Lancaster (Mass.) -- First Church, Thanksgiving sermons -- 1828 Nov. 27, Thanksgiving Day addresses -- Sermons, United States -- History -- Religious aspects -- Christianity -- Sermons, Sermons, American -- 19th century
Format: E-book

Title: An address delivered before the Massachusetts Society for the Suppression of Intemperance, May 31, 1827.
Creator: Sprague, Charles 1791-1875, Bowles and Dearborn
Abstract/Description: "Printed by request of the Society." Copyright June 5, 1827 by Bowles & Dearborn. Two states of gathering are noted: in one, the last word on page 18 is "garments;" in the other, it is "along." FAU copy edges trimmed to 23 cm., side stiched with brown cord.
PURL: http://purl.flvc.org/fau/fd/fauwsb10f14
Subject Headings: Alcoholism, Temperance -- Massachusetts -- Societies, etc, Temperance -- Societies, etc
Format: E-book

Title: An address, delivered on the third anniversary of the Washington Benevolent Society, April 30, 1814.
Creator: Bigelow, Timothy 1767-1821, Stebbins, Charles 1789-1873
Abstract/Description: By the Hon. Timothy Bigelow. Includes bibliographical references. FAU copy appears to have been trimmed to 21 cm. Washington Benevolent Society of Massachusetts
PURL: http://purl.flvc.org/fau/fd/fauwsb9f23
Subject Headings: Speeches, addresses, etc., American -- 19th century, United States -- History -- 18th century -- Sources, United States -- Politics and government -- 1812-1815, Washington, George -- 1732-1799 -- Anniversaries, etc
Format: E-book

Title: The responsibilities of a Republican government : a discourse, preached Fast Day, April 8, 1841.
Creator: Chapin, E. H. (Edwin Hubbell) 1814-1880, A. Tompkins
Abstract/Description: "Published by request." FAU copy imperfect: disbound, loose pages, all edges trimmed (to 19 cm).
PURL: http://purl.flvc.org/fau/fd/fauwsb13f8
Subject Headings: United States -- Politics and government -- 1841-1845 -- Sermons, Fast day sermons -- Massachusetts, Fast day sermons -- 1841 Apr. 8., Bible -- Ecclesiastes, IX, 18 -- Sermons, Republicanism -- United States -- Sermons, Sermons, American -- 19th century
Format: E-book

Title: A discourse delivered before the Georgia Historical Society, Savannah, on Wednesday, February 12, 1840.
Creator: Law, William, Georgia Historical Society
Abstract/Description: By William Law. Cover title: Judge Law's oration before the Georgia Historical Society, Savannah. FAU copy edges trimmed to 23 cm.; loose pages.
PURL: http://purl.flvc.org/fau/fd/fauwsb13f1
Subject Headings: Georgia -- History -- Colonial period, ca. 1600-1775, United States -- History -- Revolution, 1775-1783, Speeches, addresses, etc., American -- 19th century
Format: E-book

Title: Remarks of Hon. Miles Taylor, of Louisiana, accompanied by a letter to the editors of the Washington Union.
Creator: Taylor, Miles 1805-1873
Abstract/Description: Remarks of Honorable Miles Taylor, of Louisiana, accompanied by a letter to the editors of the Washington Union. FAU copy edges trimmed to 22 cm.
PURL: http://purl.flvc.org/fau/fd/fauwsb17f25
Subject Headings: Democratic Party (U.S.) -- History -- 19th century, Kansas -- Politics and government -- 1854-1861, Slavery -- United States -- Extension to the territories, Speeches, addresses, etc., American -- 19th century, United States -- Kansas Nebraska Act, United States -- Politics and government -- 1853-1857
Format: E-book

Title: An oration, delivered before the municipal authorities of the city of Fall River, July 4, 1860.
Creator: Adams, Charles Francis 1807-1886, Almy & Milne
Abstract/Description: By Charles Francis AdamsTitle and text within double rule borders. Includes bibliographical references. FAU copy edges trimmed to 21 cm.
PURL: http://purl.flvc.org/fau/fd/fauwsb18f35
Subject Headings: Fourth of July celebrations -- Massachusetts -- Fall River, Fourth of July orations -- 19th century, Fourth of July addresses -- 1860, Equality, Slavery -- United States, Speeches, addresses, etc., American -- 19th century, United States -- Declaration of Independence
Format: E-book

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