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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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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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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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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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Flight Ejection Tests Of The F-94 Ejection Seat Equipped with Telescoping Rails
Author(s): Hecht, Kenneth F.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1953-11
Report number: WADC TR 53-362
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Ground Tests Of A Pilot Ejection Seat Ejected Through Monolithic-, Reinforced-Monolithic-, And Laminated-Type Canopies
Author(s): Hecht, Kenneth F.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1953-10
Report number: WADC TR 53-361
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Flight Tests Of Downward And Rearward Ejected Seats Conducted with A B-29 Airplane
Author(s): Santi, Gino P.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1953-10
Report number: WADC TR 53-360
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Aircraft Ski Landing Gear Development
Author(s): Dreyer, Charles W.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1953-09
Report number: WADC TR 53-155
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Ground and Flight Tests on an Automatic-opening Lap Belt for Ejection Seats
Author(s): Hecht, K. F.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1953-12
Report number: WADC TR 53-365

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