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

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

Author(s): B. M. Leadon, G. E. Anderson
Corporate Author: Dept. Of Aeronautical Engineering, University Of Minnesota
Laboratory: Aircraft Laboratory
Date of Publication: 1953-10
Report Number: WADC TR 53-490
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The Wall Pressure Distribution In A Choked Tunnel

Author(s): Gottfried Guderley
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1953-12
Report Number: WADC TR 53-509
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Temperature Distributions In A Typical Aircraft Structure Due To Transient External Heating, Volume I, T-33 Airplane

Author(s): Alphonso Ambrosio; Bertram Bussell; William F. Macinnes
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
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Permanent Buckling Of Sheet-Stringer Panels At Elevated Temperatures

Author(s): Robert A. Needham
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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Temp-Tapes: Improved Design, Construction, And Calibration

Author(s): Alphonso Ambrosio; Bertram Busseli
Corporate Author: University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report Number: WADC TR 53-211
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An Experimental Investigation Of Hot Gas Ejectors For Boundary Layer Control

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

Author(s): Ambrose B. Nutt
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1953-04
Report Number: WADC TR 53-92
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Aeroelastic Effects On Dynamic Longitudinal Stability

Author(s): Goland, Martin; Luke, Yudell L.
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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Effects of Spring and Inertia Devices on the Longitudinal Stability of Aircraft

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

Flight Test Investigation to Determine the Effectiveness of a Rocket as an Emergency Spin Recovery Device: Phase II

Author(s): G. H. Farmer
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): Martin Goland; Tudell L. Luke; Irving Sacks
Corporate Author: Midwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1953-11
Report Number: WADC TR 53-425
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An Investigation Of The Experimental Determination Of Aircraft Inertia

Author(s): Claude R. Woodard
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report Number: WADC TR 53-207
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An Experimental Investigation of the Flutter Characteristics of a Cusp-Type Spoiler

Author(s): R. H. Schwab and G. Fotieo
Corporate Author: Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1953-01
Report Number: AF TR 5785
AD Number:
full text unavailable