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

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

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

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

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

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

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

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

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

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

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

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: