Subsonic Flow Over a Body Between Porous Walls

Author(s): Kassner, Rudolph R.
Corporate Author: Wright Air Development Center
Laboratory: Aircraft Laboratory
Date of Publication: 1952-02
Report Number: WADC TR 52-9

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

Author(s): Farmer, G. H.
Corporate Author: North American Aviation, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1952-01
Report Number: WADC TR 52-233

Rolling Effectiveness and Aileron Reversal Characteristics of Straight and Sweptback Wings: Part 3. Evaluation and Test Results

Author(s): Groth, Eric
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1952-09
Report Number: AF TR 6198 Part 3
AD Number: AD0003719

Measurements with Honeycombs in the Full-Scale and in the Model Vertical Wind Tunnel

Author(s): Knackstedt, Wilhelm F.
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1952-08
Report Number: WADC TR 52-207
AD Number: AD0008717

Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 16. Stress and Deflection Tests on Two Full Span 45 Degree Swept Plates of Different Thickness Distribution With Various Support Conditions

Author(s): Sechler, E. E.
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1952-07
Report Number: AF TR 5761 Part 16