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

J. H. Breeman

1983

Páginas: 16

Género: Static pressure

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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

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Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel

Elizabeth B. Plentovich

1986

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Rocket-based combined cycle engine technology development

J. R. DeBonis

1996

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Study of CFD methods applied to rapidly deforming boundaries

John W. Slater

1997

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Experimental cavity pressure measurements at subsonic and transonic speeds

Elizabeth B. Plentovich

1993

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Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)

E. Allen Arrington

1997

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Static presssure position error calibration of the NAE T-33 C-FSKH

J. F. Aitken

1987

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PSP measurement of stator vane surface pressures in a high speed fan

Jan Lepicovsky

1998

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