100 reports
Statistical Control System Design
Author(s): Reiss, R. Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-10 Report Number: AFFDL TR 66-83Development Design Methods for Predicting Hypersonic Aerodynamic Control Characteristics
Author(s): Popinski, Z. Corporate Author: Lockheed-California Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 66-85Time Based Analysis of Control Activities and Information Requirements for V/STOL
Author(s): Semple, Clarence A. Corporate Author: Bunker-Ramo Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-06 Report Number: AFFDL TR 65-193
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Sonic Fatigue in Combined Environment
Author(s): Ballantine, John R. Corporate Author: Lockheed-Georgia Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-05 Report Number: AFFDL TR 66-7
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Design and Performance of a 15 KW Wide Band Acoustic Facility
Author(s): Hankel, Keith M. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-03 Report Number: AFFDL TR 66-8Matrix Methods in Structural Mechanics
Author(s): Przemieniecki, J. S. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL TR 66-80
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Aerodynamic Characteristics of Non-Straight-Taper Wings
Author(s): Benepe, David B. Corporate Author: General Dynamics Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-10 Report Number: AFFDL TR 66-73
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Opening Remarks
Author(s): Buck, George T. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 1Welcome Address
Author(s): Haugen, Victor R. Corporate Author: Air Force Institute of Technology` Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 3-4Keynote Address
Author(s): Pinson, Ernest A. Corporate Author: Office of Aerospace Research Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 5-7Continua and Discontinua
Author(s): Argyris, J. H. Corporate Author: University of London; University7 of Stuttgart Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 9-189A Regularization Method for Calculation of Stresses, Deformations, and Elastic Modes
Author(s): Falconer, Robert W. Corporate Author: North American Aviation, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 191-204A Survey of Analysis of Shells by the Displacement Method
Author(s): Jones, R.E. Corporate Author: The Boeing Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 205-229Development of Advanced Structural Optimization Programs and their Application to Large Order Systems
Author(s): Gellatly, Ronald A. Corporate Author: Textron's Bell Aerospace Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 231-251Automated Stress Analysis Using Substructures
Author(s): Taig, I.C. Corporate Author: British Aircraft Corporation (Operating) Limited Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 253-274A Study of the Matrix Displacement Method as Applied to Shells of Revolution
Author(s): Klein, Stanley Corporate Author: Aerospace Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 275-298The Linear Elastic Dynamic Analysis of Shells of Revolution by the Matrix Displacement Method
Author(s): Klein, Stanley Corporate Author: Aerospace Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 299-328The Equivalence of Force and Displacement Methods in the Matrix Analysis of Elastic Structures
Author(s): Kosk, Eryk Corporate Author: National Aeronautical Establishment Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 329-351Structural Influence Coefficients for a Redundant System Including Beam-Column Effects
Author(s): Rodden, William P. Corporate Author: North American Aviation, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 353-383Orthogonalization of Internal Force and Strain Systems
Author(s): Filho, Fernando Venancio Corporate Author: Instituto Technologico de Aeronautica Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 385-393Modified Potential Energy Mass Representations for Frequency Prediction
Author(s): Melosh, Robert J. Corporate Author: Philco Corporation; Jet Propulsion Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 445-455Element Stiffness-Matrices for Boundary Compatibility and for Prescribed Boundary Stresses
Author(s): Pian, Theodore H. H. Corporate Author: Massachusetts Institute of Technology Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 457-477Dynamic Stiffness Matrix Formulation by Means of Hermitian Polynomials
Author(s): Pestel, Eduard C Corporate Author: Technische Hochschule Hannover Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 479-502A Flat Triangular Shell Element Stiffness Matrix
Author(s): Melosh, Robert J. Corporate Author: Philco Western Development Laboratry Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 503-514Finite Element Stiffness Matrices for Analysis of Plate Bending
Author(s): Clough, Ray W. Corporate Author: University of California, Berkeley; The Boeing Compnay Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 515-545Triangular Elements in Plate Bending - Conforming and Non-Conforming Solutions
Author(s): Bazeley, G. P. Corporate Author: Rolls-Royce Ltd.; University of Wal;es, Swansea Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 547-576A Bending Analysis for Plates
Author(s): Herrmann, L. R. Corporate Author: University of California, Davis Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 577-602Matrix Analysis Methods for Inelastic Structures
Author(s): Lansing, W. Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 603-633The Application of the Matrix Displacement Method in Plane Elasto-Plastic Problems
Author(s): Pope, Geoffrey G. Corporate Author: Royal Aircraft Establishment Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 635-653Matrix Analysis of Creep and Plasticity Problems
Author(s): Besseling, J. F. Corporate Author: Technological University, Delft, Netherlands Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 655-677Nonlinear Structural Analysis; Tensor Formulation
Author(s): Wissmann, J. W. Corporate Author: General Dynamics/Convair Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 679-696On the Derivation of Stiffness Matrices for the Analysis of Large Deflection and Stability Problems
Author(s): Martin, Harold C Corporate Author: University of Washington Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 697-716The Effect of Axial Loads on the Stiffness of Rigid-Jointed Plane Frames
Author(s): McMinn, S. J. Corporate Author: Manchester College of Science and Technology Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 717-726The Computation of Dynamic Response Time Histories of a System Using a Matrix Iterative Technique
Author(s): D'Ewart, Benjamin B., Jr. Corporate Author: Bell Aerosystems Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 727-742A Method for the Determination of the Matrix of Impulse Response Functions with Special Reference to Applications in Random Vibration Problems
Author(s): Lin, Y. K. Corporate Author: University of Illinois Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 743-752Numerical Approach for Wave Motions in Nonlinear Solid Media
Author(s): Ang, Alfredo H. -S. Corporate Author: University of Illinois Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 753-778Quadratic Matrix Equations for Determining Vibration Modes and Frequencies of Continuous Elastic Systems
Author(s): Przemieniecki, J. S. Corporate Author: Air Force Institute of Technology Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 779-802Truncation Errors in Natural Frequencies as Computed by the Method of Component Mode Synthesis
Author(s): Hurty, Walter C. Corporate Author: Jet Propulsion Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 803-821Improved Linear Axisymetric Shell-Fluid Model for Launch Vehicle Longitudinal Response Analysis
Author(s): Archer, J. S. Corporate Author: TRW Systems Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 823-847Vibration Analysis of a Cantlievered Square Plate by the Stiffness Matrix Method
Author(s): Best, G. C. Corporate Author: General Dynamics Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 849-860Bending and Stretching of Plates Special Models for Upper and Lower Bounds
Author(s): de Veubeke, B. Fraejis Corporate Author: Universities of Liege and Louvain Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 861-886Matrix Error Analysis for Engineers
Author(s): Rosanoff, R. A. Corporate Author: North American Aviation, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 887-910Examples of Solution Accuracy in Certain Large Simultaneous Equation Systems
Author(s): Gatewood, B. E. Corporate Author: Ohio State University; North American Aviation, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 911-924A Finite Element-Method for the Determination of Non-Stationary Temperature Distribution and Thermal Deformations
Author(s): Visser, W. Corporate Author: Technological University, Delft, Netherlands Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. 925-943A Fortran IV Program To Derive The Equations Of Motion Of Systems
Author(s): Westerwick, Robert A. Corporate Author: General Dynamics/Convair San Diego Calif Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 65-194Modeling Techniques for Sonic Fatigue Prediction
Author(s): Wang, P. Corporate Author: North American Aviation, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-06 Report Number: AFFDL TR 65-171Table of Contents
Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-11 Report Number: AFFDL-TR-66-80 p. i-viiDevelopment of Improved Structural Dynamic Analysis: Volume I: General Survey
Author(s): Coale, C. W. Corporate Author: Lockheed Missiles & Space Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-10 Report Number: AFFDL TR 66-187 Volume I
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Human Engineering Support to Air Force Flight Control and Flight Display Integration Program
Author(s): Rabideau, Gerald F. Corporate Author: The Bunker-Ramo Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-10 Report Number: AFFDL TR 66-157
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