Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available