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- 1953 (12)
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- Aircraft Laboratory (12)
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12 reports
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
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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
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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
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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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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
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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
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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
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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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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
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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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