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Permanent Buckling Of Sheet-Stringer Panels At Elevated Temperatures
Author(s): Needham, Robert A.
Corporate Author(s): 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, Busseli, Bertram
Corporate Author(s): 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(s): 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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An Investigation Of The Experimental Determination Of Aircraft Inertia
Author(s): Woodard, Claude R.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-207
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Boundary Layer Control On 64A006 And 64A010 Airfoils At High Subsonic Speeds
Author(s): Leadon, B. M. , Anderson, G. E.
Corporate Author(s): 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(s): 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, Bussell, Bertram, Macinnes, William F.
Corporate Author(s): 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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Aeroelastic Effects On Dynamic Longitudinal Stability
Author(s): Goland, Martin, Luke, Yudell L.
Corporate Author(s): 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(s): 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, Luke, Tudell L., Sacks, Irving
Corporate Author(s): Midwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1953-11
Report number: WADC TR 53-425

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