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State of the Art for V/STO Control Display
Corporate Author: Lear Siegler, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1963-10 Report Number: RTD TDR 63-4167
full text by request
Nonlinear Thermoelasitc Effects on Hypersonic Stability and Control, Part III: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing
Author(s): Batt, James R. Corporate Author: Bell Aerosystems Co. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-02 Report Number: FDL TDR 64-16 Part 3
Pressure and Heat Transfer Measurements for Flows Ahead of Ramps Part III: Mach 8 Pressure Data for Flows Ahead of Ramps: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G. Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1963-12 Report Number: ASD TDR 63-679 Part 3
full text by request
Evaluation Tests for Statistical Analyzers
Author(s): Kelly, R. D. Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-06 Report Number: AFFDL TR 65-93
Systems for the Collection and Analysis of Dynamic Data
Author(s): Kelly, R. D. Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-08 Report Number: AFFDL TR 65-94
A Study of Conventional Airplane Handling Qualities Requirements: Part I. Roll Handling Qualities
Author(s): Ashkenas, I. L. Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11 Report Number: AFFDL TR 65-138 Part 1
A Study of Conventional Airplane Handling Qualities Requirements: Part II. Lateral-Directional Oscillatory Handling Qualities
Author(s): Ashkenas, I. L. Corporate Author: Systems Technology, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11 Report Number: AFFDL TR 65-138 Part 2
An Evaluation of Procedures for Calculating Aerodynamic Loads
Author(s): Schindel, Leon H. Corporate Author: Massachusetts institute of Technology Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-05 Report Number: AFFDL TR 65-18
Table of Contents
Corporate Author: IBM San Jose Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11-01 Report Number: AFFDL TR 65-145 p. i-iv
Introduction
Corporate Author: IBM San Jose Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11-01 Report Number: AFFDL TR 65-145 p. 1-4
Application of Lyapunov's Direct Method to Stability Problems in Elastic and Aeroelastic Systems
Author(s): Wang, P. K. C. Corporate Author: IBM San Jose Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11-01 Report Number: AFFDL TR 65-145 p. 29-64
Asymptotic Stability of Equilibrium of a Simplified Aerodynamic Vehicle with Flexible Tail
Author(s): Wang, P. K. C. Corporate Author: IBM San Jose Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11-01 Report Number: AFFDL TR 65-145 p. 65-71
Stability Analysis of a Simplified Pitch-Controlled Flexible Aerodynamic Vehicle Via Lyapunov's Direct Method
Author(s): Wang, P. K. C. Corporate Author: IBM San Jose Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11-01 Report Number: AFFDL TR 65-145 p. 72-83
Optimum Control of a Class of Mixed Distributed and Lumped Parameter Systems
Author(s): Wang, P. K. C. Corporate Author: IBM San Jose Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11-01 Report Number: AFFDL TR 65-145 p. 84-106
Theory of Stability and Control for Distributed Parameter Systems. An Annotated Bibliography
Author(s): Wang, P. K. C. Corporate Author: IBM San Jose Research Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-11-01 Report Number: AFFDL TR 65-145 p. 141-164
Ground Simulator Evaluations of Coupled Roll-Spiral Mode Effects on Aircraft Handling Qualities
Author(s): Newell, F. D. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-03 Report Number: AFFDL TR 65-39
Weight Minimization of Honeycomb Heat Shields
Author(s): Achard, Robert T. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-06 Report Number: AFFDL TR 65-66
Development Of Aircraft Shock Absorbers Using Friction As The Energy Dissipator
Author(s): Fricker, Walter W. Corporate Author: Cleveland Pneumatic Co OH Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1965-10 Report Number: AFFDL TR 65-96
Format-Fortran Matrix Abstraction Technique. Volume V - Supplement I. Engineering User and Technical Report - Extended.
Author(s): Pickard, J. Corporate Author: Douglas Aircraft Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-08 Report Number: AFFDL TR 66-207 Volume V Supplement I
Format-Fortran Matrix Abstraction Technique. Volume VI. Supplement I. Description of Digital Computer Program. Phase I. Extended.
Author(s): Morris, R.C. Corporate Author: Douglas Aircraft Company, Long Beach, California Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-08 Report Number: AFFDL TR 66-207 Volume VI Supplement I
Format-Fortran Matrix Abstraction Technique. Volume VII - Supplement I. Description of Digital Computer Program - Phase III - Extended.
Author(s): Frank, J. A. Corporate Author: Douglas Aircraft Company, Long Beach, California Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1970-08 Report Number: AFFDL TR 66-207 Volume VII Supplement I
Format - Fortran Matrix Abstraction Technique. Volume V. Engineering User And Technical Report.
Author(s): Pickard, J. Corporate Author: Douglas Aircraft Company, Aircraft Division Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1968-12 Report Number: AFFDL TR 66-207 Volume V
The Development And Evaluation Of The Cal/Air Force Dynamic Wind-Tunnel Testing System. Part II. Dynamic Tests Of An F-104 Model.
Author(s): Statler, Irving C. Corporate Author: Cornell Aeronautical Lab Inc Buffalo N Y Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1967-02 Report Number: AFFDL TR 66-153 Part 2
Low Pressure Type Expandable Aircraft Tire Characteristics
Author(s): Wagner, Paul M. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1967-03 Report Number: AFFDL TR 66-170
Flight Evaluation of Various Phugoid Dynamics and 1/Th1 Values for the Landing Approach Task
Author(s): Chalk, Charles Corporate Author: Cornell Aeronutical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-02 Report Number: AFFDL TR 66-2
Mathematical Analysis of Heat Conduction in a Sector of a Hollow Circular Cylinder
Author(s): None Given Corporate Author: Martin Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 66-16
Fundamental Relationships for Ablation and Hyperthermal Heat Transfer
Author(s): Achard, Robert T. Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-04 Report Number: AFFDL TR 66-25
Aircraft Ground-Flotation Investigation: Part V - Data Report on Test Section 4
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-43 Part 5
Aircraft Ground-Flotation Investigation: Part VII - Data Report on Test Section 6
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-43 Part 7
Aircraft Ground-Flotation Investigation: Part VIII - Data Report on Test Section 7
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-08 Report Number: AFFDL TR 66-43 Part 8
Aircraft Ground-Flotation Investigation: Part X - Data Report on Test Section 9
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 66-43 Part 10
Aircraft Ground-Flotation Investigation: Part XI - Data Report on Test Section 10
Author(s): Brabston, W. Corporate Author: U. S. Army Engineer Waterways Experiment Station Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-09 Report Number: AFFDL TR 66-43 Part 11
Preliminary Development of Gust Design Procedures Based on Power Spectral Techniques: Volume I - Theoretical and General Considerations
Author(s): Houbolt, John C. Corporate Author: Aeronautical Research Associates of Princeton, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-07 Report Number: AFFDL TR 66-58 Volume 1
A 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. 925-943
Atmospheric Turbulence Spectra From B-52 Flight Loads Data
Author(s): Coy, Richard G. Corporate Author: Dayton Univ OH Research Inst Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1967-04 Report Number: AFFDL TR 67-13
The Method Of Characteristics For Three-Dimensional Real-Gas Flows Including The Digital Computer Program Details And Operating Procedures For Frozen Flows.
Author(s): Strom, Charles R. Corporate Author: Cornell Aeronautical Lab Inc Buffalo N Y Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1967-07 Report Number: AFFDL TR 67-47
Experimental Flight Instruments
Author(s): Schouten, Tunis H. Corporate Author: Lear Siegler Inc Grand Rapids Mi Instrument Div Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1967-12 Report Number: AFFDL TR 67-143
Wind Tunnel Studies Of The Pressure Distribution And The Flow Field In The Wake Of The Lockheed C-141A Starlifter Jet Transport Aircraft
Author(s): Goodrick, T. F. Corporate Author: Minnesota Univ Minneapolis Dept Of Aeronautics And Engineering Mechanics Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1968-05 Report Number: AFFDL TR 67-163
Prediction Of Boundary Layer Pressure Fluctuations
Author(s): Lowson, Martin V. Corporate Author: Wyle Labs Inc Huntsville AL Testing Div Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1968-04 Report Number: AFFDL TR 67-167
Establishment Of An Unsymmetrical Wake Test Capability For Aerodynamic Decelerators. Volume III. Experimental Wake Survey And Body Surface Pressure Data
Author(s): Henke, Daniel W. Corporate Author: Goodyear Aerospace Corp Akron Ohio Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1968-08 Report Number: AFFDL TR 67-192 Volume 3
Iterative Method For The Analysis Of Large Structural Systems
Author(s): Venkayya, V. B. Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB Ohio Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1968-04 Report Number: AFFDL TR 67-194
Preliminary Development of Gust Design Procedures Based on Power Spectral Techniques: Volume II - Summary of Possible Procedures
Author(s): Houbolt, John C. Corporate Author: Aeronautical Research Associates of Princeton, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1966-07 Report Number: AFFDL TR 66-58 Volume 2
Continua 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. 9-189
Automated 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. 253-274
A 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. 275-298
The 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. 329-351
Structural 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. 353-383
Orthogonalization 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. 385-393
Element 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. 457-477
Dynamic 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. 479-502