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Book dossier
by J. H. Breeman
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Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
Richard J. Re
Rocket-based combined cycle engine technology development
J. R. DeBonis
Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel
Elizabeth B. Plentovich
Study of CFD methods applied to rapidly deforming boundaries
John W. Slater
Static presssure position error calibration of the NAE T-33 C-FSKH
J. F. Aitken
Analysis of fluctuating static pressure measurements in the National Transonic Facility
William B. Igoe
Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)
E. Allen Arrington
A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
A preliminary look at techniques used to obtain airdata from flight at high angles of attack
Timothy R. Moes
