Limit your search
Tags
Publication Date
Laboratory
Report Availability
614 reports
Fixed-Base and In-Flight Simulations of Longitudal and Lateral-Directional Handling Qualities for Piloted Re-Entry Vehicles
Author(s): Edwin A. Kidd, Robert P. Harper, Jr. Corporate Author: Cornell Aeronautical Laboratory, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 2/1/1964 Report Number: ASD TDR 61-362
Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part I. Expansion Corner Flows. Part Of An Investigation Of Hypersonic Flow Separation And Control Characteristics
Author(s): Louis G. Kaufman II Corporate Author: Grumman Aircraft Engineering Corp Bethpage N Y Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 10/1/1963 Report Number: RTD TDR 63-4044 Part 1
full text by request
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: 12/1/1963 Report Number: ASD TDR 63-679 Part 3
full text by request
Functional Capability of Neuromime Networks for Use in Attitude Stabilization Systems
Author(s): R. J. Lee; R. F. Snyder Corporate Author: Adaptronics, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 9/1/1963 Report Number: ASD TDR 63-549
full text by request
Determination of Thermal and Mechanical Loadings on Aerospace Vehicles, Volume I.
Author(s): Makemson, Richard L. and Beaumont, Saul S. Corporate Author: Republic Aviation Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 9/1/1963 Report Number: ASD TDR 63-852 Volume 1
full text by request
Analysis of the Probability of Collapse of a Fail-Safe Aircraft Structure Consisting of Parallel Elements
Author(s): S. Eggwertz; G. Lindsjo Corporate Author: Aeronautical Research Institute of Sweden Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 2/1/1964 Report Number: RTD TDR 63-4210
State of the Art for V/STO Control Display
Corporate Author: Lear Siegler, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 10/1/1963 Report Number: RTD TDR 63-4167
full text by request
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part II" Pressure Data for Dihedral Surfaces Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Louis G. Kaufman II Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 9/1/1964 Report Number: FDL TDR 64-2 Part 2
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): James R. Batt Corporate Author: Bell Aerosystems Co. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 2/1/1965 Report Number: FDL TDR 64-16 Part 3
Transient Dynamic Response of Orbiting Space Stations
Author(s): C. L. Tai, L. V. Andrew, M. M. H. Loh, P. C. Kamrath Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 2/1/1965 Report Number: FDL TDR 64-25
Confac II, A General Computer Program for the Determination of Radiant-Interchange Configuration and Form Factors
Author(s): Kempton A. Toups Corporate Author: North American Aviation, Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 4/1/1964 Report Number: FDL TDR 64-43
Development of Frontal Section for Super-Orbital, Lifting, Re-Entry Vehicle, Volume II: Materials and Composite Structure Development
Author(s): M. R. Licciardello, B. Ohnysty, and A. R. Stetson Corporate Author: International Harvester Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/29/1964 Report Number: FDL TDR 64-59 Volume 2
Development of Frontal Section for Super-Orbital, Lifting, Re-Entry Vehicle, Volume III: Asset Nose Cap
Author(s): M. R. Licciardello Corporate Author: International Harvester Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/29/1964 Report Number: FDL TDR 64-59 Volume 3
High Vacuum Measuring Instrumentation and Methodology
Author(s): Jonathan R. Roehrig Corporate Author: National Research Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 4/1/1964 Report Number: FDL TDR 64-68
A Conical Thin-Shock-Layer Theory Uniformly Valid in the Entropy Layer
Author(s): Robert E. Melnik Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1/1/1965 Report Number: FDL TDR 64-82
Energy Dissipation at Structural Joints; Mechanisms and Magnitudes
Author(s): Eric E. Ungar Corporate Author: Bolt Beranek and Newman Inc. Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 8/1/1964 Report Number: FDL TDR 64-98
Pressure and Heat Transfer Measurements at Mach 13 and 19 for Flows Ahead of Ramps, Over Expansion Corners, and Past Fin-Plate Combinations: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Stavros A. Hatofilis Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 9/1/1964 Report Number: FDL TDR 64-144
Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps. Part IV: Mach 8 Heat Transfer 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 Coporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 7/1/1964 Report Number: ASD TDR 63-679 Part 4
full text by request
Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part II. Conical Cabin Configuration
Author(s): Kaufman,Louis G., II Corporate Author: Grumman Aircraft Engineering Corp Bethpage N Y Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 2/1/1964 Report Number: RTD TDR 63-4179 Part 2
full text by request
Development Of Frontal Section For Super-Orbital, Lifting, Re-Entry Vehicle. Volume I. Trajectory And Vehicle Analyses
Author(s): Jacobsen, W. E.; Licciardello, M. R. Corporate Author: Solar Turbines International San Diego CA Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/29/1964 Report Number: RTD TDR 64-59 Volume 1
Design Analysis Summary Of Two Force-Balance Hypersonic Inlet Configurations
Author(s): Kutschenreuter, Paul H., Jr.; Balent, Richard L.; Richy, George K. Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson Afb Ohio Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 3/1/1964 Report Number: FDL TDR 64-19
Research and Development of a Hot Gas Flight Stabilization System
Author(s): R. E. Feucht; L. B. Taplin; R. Bosworth; A. Gregory; G. MacArthur Corporate Author: Bendix Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 2/1/1964 Report Number: WADD TR 60-449 Part 4
full text unavailable
Six-Degree-of-Freedom Flight-Path Study Generalized Computer Program: Part I. Problem Formulation
Author(s): Robert C. Brown; Robert V. Brulle; A. E. Combs; Gerald D. Griffin Corporate Author: McDonnell Aircraft Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 10/1/1964 Report Number: FDL TDR 64-1 Part 1 Volume 1
Pressure Measurements for Mach Five Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Louis G. Kaufman II Corporate Author: Grumman Aircraft Engineerign Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1/1/1964 Report Number: RTD TDR 63-4239
full text by request
An Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Louis G. Kaufman II; Lawrence Meckler; Stavros A. Hartofilis; Daniel Weiss Corporate Author: Grumman Aircraft Engineerign Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1/1/1965 Report Number: AFFDL TR 64-174
Unsteady Aerodynamics for Advanced Configurations: Part V - Unsteady Potential Flow Around Slender Bodies at Angles of Attack
Author(s): T. C. Li Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/1/1965 Report Number: FDL TDR 64-152 Part 5
Unsteady Aerodynamics for Advanced Configurations: Part IV - Application of the Supersonic Mach Box Method to Intersecting Planar Lifting Surfaces
Author(s): M. T. Moore; L. V. Andrew Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/1/1965 Report Number: FDL TDR 64-152 Part 4
Unsteady Aerodynamics for Advanced Configurations: Part II - A Transonic Box Method for Planar Lifting Surfaces
Author(s): E. R. Rodemich; L. V. Andrew Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/1/1965 Report Number: FDL TDR 64-152 Part 2
Unsteady Aerodynamics for Advanced Configurations: Part I - Application of the Subsonic Kernel Function to Nonplanar Lifting Surfaces
Author(s): H. T. Vivian; L. V. Andrews Corporate Author: North American Aviation, Incorporated Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/1/1965 Report Number: FDL TDR 64-152 Part 1
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part I: Pressure Data for Delta Wing Surface
Author(s): Louis G. Kaufman II Corporate Author: Grumman Aircraft Engineerign Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1/1/1964 Report Number: FDL TDR 64-2 Part 1
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part III: Heat Transfer Data for Delta Wing Surface
Author(s): Louis G. Kaufman II Corporate Author: Grumman Aircraft Engineerign Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/1/1964 Report Number: FDL TDR 64-2 Part 3
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part IV: Heat Transfer Data for Dihedral Surfaces Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Louis G. Kaufman II Corporate Author: Grumman Aircraft Engineerign Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/1/1964 Report Number: FDL TDR 64-2 Part 4
A Survey of Aerodynamic Noise
Author(s): J. D. Ingram Corporate Author: General Technology Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 12/1/1964 Report Number: FDL TDR 64-132
Theoretical Studies of Methods of Generating Random Waves from Harmonic Sources
Author(s): J. C. Samuels Corporate Author: General Technology Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 12/1/1964 Report Number: FDL TDR 64-133
Aerodynamic Characteristics and Flap Loads for a Blunt Pyramidal Configuration at Mach 5 and 8: :Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): William J. Evans; Louis G. Kaufman II Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 9/1/1964 Report Number: FDL TDR 64-128
Aircraft Motion Analysis
Author(s): J. A. Thelander Corporate Author: Douglas Aircraft Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 3/1/1965 Report Number: FDL TDR 64-70
Theoretical Investigations of Boundary Layer Stability
Author(s): Gibbs S. Raetz; W. Byron Brown Corporate Author: Northrop Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 9/1/1966 Report Number: AFFDL TR 64-184
Active Control of Booster Elasticity
Author(s): Robert L. Swaim Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 4/1/1965 Report Number: AFFDL TR 64-189
Response of Elastic Structures to Deterministic and Random Excitation
Author(s): R. L. Barnoski Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 5/1/1965 Report Number: AFFDL TR 64-199
Six-Degree-of-Freedom Flight Path Study Generalized Computer Program: Part II, Volume 2 - User's Manual for Part I, Volume 2
Author(s): J. L. Harris, J. A. Shilling and R. F. Vorwald Corporate Author: McDonnell Aircraft Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 10/1/1964 Report Number: FDL TDR 64-1 Part 2 Volume 2
full text by request
Window Systems for Advanced Vehicles
Author(s): S. J. Lis, R. G. Barile and G. Engholm Corporate Author: General American Transportation Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 12/1/1964 Report Number: FDL TDR 64-39
Dynamic Buckling of Shell Structures Subject to Longitudinal Impact
Author(s): A. P. Coppa and W. A. Nash Corporate Author: General Electric Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 12/1/1964 Report Number: FDL TDR 64-65
Methods in Structural Dynamics for Thin Shell Clustered Launch Vehicles
Author(s): J. S. Keith and J. W. Lincoln Corporate Author: LTV Astronautics Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 4/1/1965 Report Number: FDL TDR 64-105
Aerodynamic Heating Simulation: Part I. Theory and Program Definition
Author(s): Glendon R. Crump, Lt, USAF Corporate Author: Air Force Flight Dynamics Laboratory Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 9/1/1964 Report Number: FDL TDR 64-112 Part 1
Development of an Advanced Digital Adaptive Flight Control System
Author(s): J. Zaborszky, W. J. Luedde, R. L. Berger, J. B. Berger and M. A. Madonna Corporate Author: McDonnell Aircraft Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 12/1/1964 Report Number: FDL TDR 64-115
full text by request
An Analysis of Amplitude Probability Measurements
Author(s): G. P. Thrall Corporate Author: Measurement Analysis Corporation Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 3/1/1965 Report Number: FDL TDR 64-116
Stress Analysis of a Parachute During Inflation and at Steady State
Author(s): Helmut G. Heinrich and Lelan R. Jamison, Jr. Corporate Author: University of Minnesota Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 2/1/1965 Report Number: FDL TDR 64-125
Thermal Response in Sandwich Panels
Author(s): P. Kendall Corporate Author: Martin Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 10/1/1964 Report Number: FDL TDR 64-135
full text by request
Hypersonic Dynamic Stability: Part II. Conical Body Experimental Program
Author(s): R. B. Hobbs, Jr. Corporate Author: General Electric Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1/1/1967 Report Number: FDL TDR 64-149 Part 2
Hypersonic Dynamic Stability: Part III. Unsteady Flow Field Program
Author(s): H. Rie, E. A. Linkiewicz and F. D. Bosworth Corporate Author: General Electric Company Laboratory: Air Force Flight Dynamics Laboratory Date of Publication: 1/1/1967 Report Number: FDL TDR 64-149 Part 3