Analysis of fluctuating static pressure measurements in the National Transonic Facility

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

Method for determining the time delay of the pitot-static tubing system of aircraft

J. H. Breeman

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

Richard J. Re

A preliminary look at techniques used to obtain airdata from flight at high angles of attack

Timothy R. Moes