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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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The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges
Author(s): Epstein, Melvin
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Report number: WADC TR 54-196
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On The Flow Over A Finite Wedge In The Lower Transonic Region
Author(s): Yoshihara, Hideo
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-444
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Spin And Recovery Test Of A 1/20 -scale Model Of The Cessna XT-37 Airplane
Author(s): Knackstedt, Wilhelm F., Sury, John J.
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1957-09
Report number: WADC TR 57-584
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Management Briefing on Low Drag Boundary Layer Control
Author(s): Flatt, Joseph, Klepinger, Richard H.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1956-11-08
Report number: WADC TR 56-662
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Performance Of Flared Exhaust Ducts Suitable For Jet Flap Applications
Author(s): Lopiccolo, Robert C., Nelsen, Raymond Z., Jr., Palm-Leis, Ahto
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1958-04
Report number: WADC TR 57-592

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