Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate at a Mach number of 5
By: Tony L. Parrott, Michael G. Jones, Cindy W. Albertson.
Contributors: Jones, Michael G.; Albertson, Cindy W.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical paper -- 2947.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 36
Subjects: Aerodynamic load -- Measurement.; Turbulent boundary layer.; Aerodynamics, Hypersonic.; High temperature.; Mach number.; Piezoresistive transducers.; Pressure measurement.; Signal processing.; Turbulent boundary layer.
Notes: Research done at Langley Research Center.

Shipping list no.: 90-0370-M.

Includes bibliographical references (p. 16-17).

Also available via Internet from the NASA Technical Report Server web site. Address as of 4/10/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900001364%5F1990001364.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989]. 1 microfiche.