Cover Image

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
Description
Item Description:"November 1989"
Research done at Langley Research Center.
Shipping list number: 90-0370-M.
Microform.
Physical Description:36 pages : illustrations ; 28 cm.
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.
Bibliography:Includes bibliographical references (pages 16-17).