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Response Of Helicopter Rotors To Oscillatory Rotor Plane Drag Forces At The Blades
Author(s): Rogers, Orville R., Oleksak, William
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1952-09
Report number: WADC TR 52-270
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Aerodynamic Noise And The Estimation Of Noise In Aircraft
Author(s): Rogers, Orville R., Cook, Robert F.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1952-02
Report number: WADC TR 52-341
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Rolling Effectiveness and Aileron Reversal Characteristics of Straight and Sweptback Wings: Part 3. Evaluation and Test Results
Author(s): Groth, Eric
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1952-09
Report number: AF TR 6198 Part 3
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Measurements with Honeycombs in the Full-Scale and in the Model Vertical Wind Tunnel
Author(s): Knackstedt, Wilhelm F.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1952-08
Report number: WADC TR 52-207
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Flight Tests Of The F-84D Ejection Seat
Author(s): Hecht, K. F.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1950-12
Report number: WADC TR 53-366
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Wind Tunnel Tests of the Coanda Wing and Nozzle
Author(s): Young, D. W., Zonars, D.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1950-09
Report number: AF TR 6199
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Investigation Of Aerodynamic Forces Generated By A Propeller In A Compressible Flow
Author(s): Lieber, Paul, Wan, Koon-San, Spiegel, M.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1955-09
Report number: WADC TR 55-312
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Wall Corrections For A wing Near A Ground Plate In A Circular Cross Section wind Tunnel
Author(s): Albritton, J. P., Huber, F. J. A.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1955-06
Report number: WADC TR 55-280
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Unsteady Laminar Heat Transfer From A Flat Plate
Author(s): Yoshihara, Hideo
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1955-10
Report number: WADC TR 55-370
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Subsonic Flutter Tests of an Unswept All-Movable Horizontal Tail
Author(s): Hoffman, Niles R., Spielberg, Irvin N.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-53

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