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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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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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Method For Predicting Dynamic Landing Loads
Author(s): Eisenman, Richard L., Kramer, Edward H.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-09
Report number: WADC TR 54-28
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Effects Of The Upstream Influence Of A Shock wave At Supersonic Speeds In The Presence Of A Separated Boundary Layer
Author(s): Daniels, Lloyd E., Yoshihara, Hideo
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1954-01
Report number: WADC TR 54-31
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Gunfire Tests On Transparent Panels
Author(s): Riley, James L.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1954-10
Report number: WADC TR 54-461
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Snow As It Affects Aircraft Ski Performance
Author(s): Thompson, Thomas L.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1953-06
Report number: WADC TR 53-154
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Transonic Simplifications Of The Hodograph Equation
Author(s): Guderley, Gottfried
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1953-06
Report number: WADC TR 53-183

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