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.

Limit your search

Publication Date

Report Availability

20 reports

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
full text available

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
full text available

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
full text available

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
full text available

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
full text available

Preliminary Development of a Solid-State Matrix Display

Author(s): Lechner, B. J.
Corporate Author: Radio Corporation of America
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-01
Report Number: AFFDL TR 66-5
full text available

Development And Experimental Evaluation Of A Retrieval System For Air Force Control-Display Information.

Author(s): Debons, Anthony
Corporate Author: Dayton Univ Ohio Research Inst
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-11
Report Number: AFFDL TR 67-119
full text available

Investigation Of Ablation Effects On Hypersonic Dynamic Stability Of A 10 Deg. Cone.

Author(s): Moore, Dave R.
Corporate Author: LTV Aerospace Corp Dallas Tex LTV Vought Aeronautics Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-01
Report Number: AFFDL TR 66-230
full text available

Basis Of A Well Conditioned Force Program For Equilibrium Models Via The Southwell Slab Analogies

Author(s): de Veubeke, Baudouin M. Fraeijs
Corporate Author: Liege Univ (Belgium) Laboratoire D'aeronautique
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-03
Report Number: AFFDL TR 67-10
full text available

Investigation of Turbulent Heat Transfer at Hypersonic Speeds. Volume I. Analytical Methods.

Author(s): Savage, Richard T.
Corporate Author: Boeing Company Aerospace Group, Seattle, Washington
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-12
Report Number: AFFDL TR 67-144 Volume 1
full text available

Design, Fabrication, and Ground Testing of the F-4 Beryllium Rudder

Author(s): Finn, J. M.
Corporate Author: McDonnell Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-04
Report Number: AFFDL TR 67-68
full text available

Adaptive Characteristics of the Human Controller of Time-Varying Systems

Author(s): Elkind, Jerome I.
Corporate Author: Bolt Beranek and Newman Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-12
Report Number: AFFDL TR 66-60
full text available

Self-Regulated Oxygen Concentrator

Author(s): Mrava, G. L.
Corporate Author: TRW Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-03
Report Number: AFFDL TR 67-6
full text available

Hypersonic Dynamic Stability: Part III. Unsteady Flow Field Program

Author(s): Rie, H.
Corporate Author: General Electric Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-01
Report Number: FDL TDR 64-149 Part 3
full text available

Effects of Gust Velocity Spatial Distributions on Lateral-Directional Response of a VTOL Aircraft

Author(s): Swaim, Robert L.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-06
Report Number: AFFDL TR 67-93
full text available

The Development And Evaluation Of The Cal/Air Force Dynamic Wind-Tunnel Testing System. Part I. Description And Dynamic Tests Of An F-80 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 1
full text available

Analysis and Experiment of Radiant Heat Exchange Between Simply Arranged Surfaces

Author(s): Viskanta, R.
Corporate Author: School of Mechanical Engineering, Purdue University
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-07
Report Number: AFFDL TR 67-94
full text available

Pressure distribution Measurements on Several Rigid Hyperflo Models at Mach 3.0 and 4.0

Author(s): Noreen, R. A.
Corporate Author: University of Minnesota
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-09
Report Number: AFFDL TR 67-84
full text available

Hypersonic Dynamic Stability: Part II. Conical Body Experimental Program

Author(s): Hobbs, R. B., Jr.
Corporate Author: General Electric Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-01
Report Number: FDL TDR 64-149 Part 2
full text available

Aircraft Ground-Flotation Investigation Part I - Basic Report

Author(s): Ladd, D.
Corporate Author: U. S. Army Waterways Experiment Station
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-08
Report Number: AFFDL TR 66-43 Part I
full text available