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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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Upward Ejection Seat Flight Tests Utilizing The M4 Catapult
Author(s): Hecht, K. F.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1953-12
Report number: WADC TR 53-364
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Upward Ejection Ground And Flight Tests Of Aircraft Personnel Catapult Type T-5
Author(s): Hecht, K. F.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1953-12
Report number: WADC TR 53-363
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The Wall Pressure Distribution In A Choked Tunnel
Author(s): Guderley, Gottfried
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1953-12
Report number: WADC TR 53-509
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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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