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New Standard Atmosphere: The WADC 1952 Model Atmosphere
Author(s): Williams, D. T., Nash, W. F., Bell, J. C.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-215
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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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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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