Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate at a Mach number of 5 /

Bibliographic Details
Main Author:	Parrott, Tony L.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors:	Jones, Michael G., Albertson, Cindy W.
Format:	Government Document Microform Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1989.
Series:	NASA technical paper ; 2947.
Subjects:	Aerodynamic load > Measurement. Turbulent boundary layer. Aerodynamics, Hypersonic. High temperature. Mach number. Piezoresistive transducers. Pressure measurement. Signal processing.
Online Access:	https://purl.fdlp.gov/GPO/LPS68643

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