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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42 reports

Structural Response Of Beryllium Sheet Produced By Three Fabrication Methods

Author(s): Giemza, C. J.
Corporate Author: Martin Co Baltimore Md
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report Number: ASD TR 61-87
full text by request

NB-66B High Altitude Gust Survey Technical Analysis, Volume I.

Author(s): Strom, J. A.
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-04
Report Number: ASD TDR 63-145 Volume 1
full text by request

NB-66B High Altitude Gust Survey Power Spectra, Volume II.

Author(s): Strom, J. A.
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-04
Report Number: ASD TDR 63-145 Volume 2
full text by request

NB-66B High Altitude Gust Survey Time Series, Volume III.

Author(s): Strom, J. A.
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-04
Report Number: ASD TDR 63-145 Volume 3
full text by request

Fixed-Base Simulator Investigation of the Effect of L (sub alpha) and True Speed on Pilot Opinion of Longitudinal Flying Qualities

Author(s): Chalk, Charles R.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 63-399
full text by request

Elements of Simulation Error Analysis

Author(s): Whitbeck, Richard F.
Corporate Author: Systems Technology, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1982-06
Report Number: AFWAL-TR-82-3022
full text by request

Further Studies on High-Speed Unsteady Flow

Author(s): Zartanian, Garabed
Corporate Author: Massachusetts Institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-09
Report Number: ASD TDR 62-463
full text by request

Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered

Author(s): Buck, Melving L.
Corporate Author: Aeronautical Systems Div Wright-Patterson AFB Ohio Flight Control Lab
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-08
Report Number: ASD TR 61-107
full text by request

Durability of Continuous Fiber Reinforced Metal Matrix Composites

Author(s): Harmon, D. M.
Corporate Author: McDonnell Aircraft Company and Purdue University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1987-10-01
Report Number: AFWAL-TR-87-3060
full text by request

Calibration of an Axial Fan at Various Power Settings for Use on a Quarter Scale XC-8A Air Cushion Model

Author(s): Fischer, David L.
Corporate Author: Mechanical Branch, Vehicle Equipment Division
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1980-01-01
Report Number: AFWAL TR 80-3094
full text by request

A Study of Aerodynamic Control in Stalled Flight Long Laminar Separation Bubble Analysis

Author(s): Dvorak, F. A.
Corporate Author: Analytical Methods, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1985-02-01
Report Number: AFWAL TR 84-3091
full text by request

Investigation Of Escape Capsule Systems For Multi-place Aircraft. Part II: Preliminary Design And wind Tunnel Testing Of An Individual Escape Capsule

Author(s): Milhoan, F. M.
Corporate Author: Goodyear Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report Number: WADC TR 57-329 Part 2
full text by request

Strength, Efficiency, and Design Data for Beryllium Structures

Author(s): Crawford, Robert F.
Corporate Author: Lockheed Missiles & Space Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report Number: ASD TR 61-692
full text by request

An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. I. Surface Pressure Distributions on a Blunted Flat Plate

Author(s): Gregorek, G. M.
Corporate Author: Ohio State University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-03
Report Number: ASD TDR 62-792 Volume 1
full text by request

An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. II. Laminar Boundary Layer Profile on the Flat Plate

Author(s): Gregorek, G. M.
Corporate Author: Ohio State University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-03
Report Number: ASD TDR 62-792 Volume 2
full text by request

Establishment of the Approach to, and Development of, Interim Design Criteria for Sonic Fatigue

Author(s): Fitch, G. E.
Corporate Author: North American Aviation, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-06
Report Number: ASD TDR 62-26
AD Number: AD0284597
full text by request

Proposed MIL Standard and Handbook - Flying Qualities of Air Vehicles Volume I: Proposed MIL Standard

Author(s): Ho, Roger H.
Corporate Author: Systems Technology, Inc. and McDonnell Aircraft Co.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1982-11
Report Number: AFWAL-TR-82-3081 Volume I
full text by request

Problems in Forced, Unsteady Fluid Mechanics

Author(s): Viets, Herman
Corporate Author: Wright State University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1981-11-01
Report Number: AFWAL TM 81-148-FIMM
full text by request

Investigation Of Escape Capsule Systems For Multi-place Aircraft . Part I: Preliminary Investigation

Author(s): Vorachek, J. J.
Corporate Author: Goodyear Aircraft Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-12
Report Number: WADC TR 57-329 Part 1
full text by request

Research on Techniques of Establishing Random Type Fatigue Curves for Broad Band Sonic Loading

Author(s): Fuller, J. R.
Corporate Author: The Boeing Company, Transport Division
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report Number: ASD TDR 62-501
full text by request

A Study of Aerodynamic Control in Stalled Flight Leading-Edge Vortex Formation Analysis

Author(s): Nathman, James K.
Corporate Author: Analytical Methods, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1985-02-01
Report Number: AFWAL TR 84-3090
full text by request

Advanced Acuation Systems Development

Author(s): Jenney, Gavin D.
Corporate Author: Dynamic Controls, Inc.
Laboratory: Flight Dynamics Laboratory
Report Number: WRDC-TR-89-3076 Volume I
full text by request

Advanced Actuation Systems Development

Author(s): Jenney, Gavin D.
Corporate Author: Dynamic Controls, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1989-08
Report Number: WRDC-TR-89-3076 Volume II
full text by request

Investigation of High-Angle-of-Attack Maneuver-Limiting Factors: Part I: Analysis and Simulation

Author(s): Johnston, Donald E.
Corporate Author: Systems Technology, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1980-12
Report Number: AFWAL-TR-80-3141 Part I
full text by request

Basic Research on Adaptive Model Algorithmic Control

Author(s): Larimore, Wallace E.
Corporate Author: Scientific Systems, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1985-12
Report Number: AFWAL-TR-85-3113
full text by request

Feasibility Studies on Use of Artrons as Logic Elements in Flight Control Systems

Author(s): Mirabelli, R. E.
Corporate Author: Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1964-09
Report Number: FDL TDR 64-23
full text by request

In-Flight Investigation of Large Airplane Flying Qualities for Approach and Landing

Author(s): Weingarten, Norman C.
Corporate Author: CALSPAN
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1981-09
Report Number: AFWAL-TR-81-3118
full text by request

Inspection Periods Determined from Data of Crack Development and Strength Reduction of an Aircraft Structure Using Static Analysis

Author(s): Eggwertz, Sigge
Corporate Author: The Aeronautical Research Institute of Sweden (FFA)
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-05
Report Number: ASD TDR 62-391
full text by request

Superplastic Formed and Diffusion Bonded Titanium Landing Gear Component Feasibility Study

Author(s): Wilson, Vernon E.
Corporate Author: Rockwell International, North American Aircraft Division
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1980-07-01
Report Number: AFWAL TR 80-3081
full text by request

Survey and Evaluation of Sonic Fatigue Testing Facilities

Author(s): Bianchi, Ralph A.
Corporate Author: CONESCO Consultants in Engineering Science
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-03
Report Number: ASD TR 61-185
AD Number: AD0277124
full text by request

Thermo-Structural Analysis Manual

Author(s): Forray, M. J.
Corporate Author: Republic Aviation Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report Number: WADD TR 60-517 Vol II
full text by request

Shock-Tube Measurements of Step-Blast Loads on a NASA 64A010 Airfoil

Author(s): Ruetenik, J. Ray
Corporate Author: Massachusetts Institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report Number: ASD TR 61-219
full text by request

Methods For Analyzing Flight Vehicles During The Taxi Condition

Author(s): Theisen, J. G.
Corporate Author: Lockheed-Georgia Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-01
Report Number: ASD TR 61-177
AD Number: AD0273305
full text by request

Prediction Of Creep Effects In Aircraft Structures

Author(s): Alesch, C. W.
Corporate Author: Convair, A Division of General Dynamics Corporation Engineering Department
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report Number: WADD TR 60-411 Part 2
full text by request

Theoretical And Experimental Studies On Airloads Related To Hypersonic Aeroelastic Problems Of General Slender Pointed Configurations

Author(s): Zartarian, Garabed
Corporate Author: Massachusetts Institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-04
Report Number: ASD TR 61-7
full text by request

Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part I: Equipment

Author(s): Turner, D. F.
Corporate Author: Midwest Research Institute
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-02
Report Number: WADD TR 60-470 Part I
full text by request

Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part II: Equipment Trials

Author(s): Turner, D. F.
Corporate Author: Midwest Research Institute
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-10
Report Number: WADD TR 60-470 Part II
full text by request

Admittance Techniques In high Speed Flutter Model Testing. Part I. Experimental Results

Author(s): Asher, Gifford W.
Corporate Author: Boeing Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-07
Report Number: WADD TR 61-31 Part I
full text by request

Feasibility To Determine Practicability Of Providing Mockup Improvements

Author(s): Lowe, W. F.
Corporate Author: Chance Vought Aircraft, Incorporated
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-08
Report Number: WADD TR 60-579
full text by request

The Dynamic Response of Advanced Vehicles

Author(s): Bohne, Q. R.
Corporate Author: Boeing Airplane Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-09
Report Number: WADD TR 60-518
full text by request

Prediction Of Creep Effects In Aircraft Structures

Author(s): Alesch, C. W.
Corporate Author: Convair, A Division of General Dynamics Corporation Engineering Department
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-04-15
Report Number: WADD TR 60-411 Part 1
full text by request

Similarity Studies For Dissociating Gases In Hypersonic , Low Density Flow

Author(s): Pearce, K.
Corporate Author: Flight Sciences Laboratory, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-09
Report Number: WADD TR 60-341
full text by request