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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13 reports

The Wall Pressure Distribution In A Choked Tunnel

Author(s): Guderley, Gottfried
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1953-12
Report Number: WADC TR 53-509
full text unavailable

Principles of Canopy Design For Military Aircraft

Author(s): Nutt, Ambrose B.
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1953-04
Report Number: WADC TR 53-92
full text unavailable

An Investigation Of The Experimental Determination Of Aircraft Inertia

Author(s): Woodard, Claude R.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report Number: WADC TR 53-207
full text unavailable

Temp-Tapes: Improved Design, Construction, And Calibration

Author(s): Ambrosio, Alphonso
Corporate Author: University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report Number: WADC TR 53-211
full text unavailable

Temperature Distributions In A Typical Aircraft Structure Due To Transient External Heating, Volume I, T-33 Airplane

Author(s): Ambrosio, Alphonso
Corporate Author: University Of California, Department Of Engineering, Los Angeles, California
Laboratory: Aircraft Laboratory
Date of Publication: 1953-04
Report Number: WADC TR 52-216
full text unavailable

Boundary Layer Control On 64A006 And 64A010 Airfoils At High Subsonic Speeds

Author(s): Leadon, B. M.
Corporate Author: Dept. Of Aeronautical Engineering, University Of Minnesota
Laboratory: Aircraft Laboratory
Date of Publication: 1953-10
Report Number: WADC TR 53-490
full text unavailable

Aeroelastic Effects On Dynamic Longitudinal Stability

Author(s): Goland, Martin
Corporate Author: Midwest Research Inst Kansas City MO
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report Number: WADC TR 53-29
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Flight Test Investigation to Determine the Effectiveness of a Rocket as an Emergency Spin Recovery Device: Phase II

Author(s): Farmer, G. H.
Corporate Author: North American Aviation, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1953-08
Report Number: WADC TR 53-396
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Effects of Airplane Elasticity and Unsteady Flow on Longitudinal Stability

Author(s): Goland, Martin
Corporate Author: Midwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1953-11
Report Number: WADC TR 53-425
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Effects of Spring and Inertia Devices on the Longitudinal Stability of Aircraft

Author(s): Goldberg, Joseph H.
Corporate Author: Princeton University
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report Number: WADC TR 53-350
full text by request

Permanent Buckling Of Sheet-Stringer Panels At Elevated Temperatures

Author(s): Needham, Robert A.
Corporate Author: University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report Number: WADC TR 53-209
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An Experimental Investigation of the Flutter Characteristics of a Cusp-Type Spoiler

Author(s): Schwab, R. H.
Corporate Author: Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1953-01
Report Number: AF TR 5785
AD Number:
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An Experimental Investigation Of Hot Gas Ejectors For Boundary Layer Control

Author(s): De Leo, Richard V.
Corporate Author: Rosemount Aeronautical Laboratories, University of Minnesota
Laboratory: Aircraft Laboratory
Date of Publication: 1953-12
Report Number: WADC TR 52-128 Part 2
full text unavailable