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Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /

Bibliographic Details
Main Author: Johnson, William G. (William Garland), 1944-
Corporate Author: Langley Research Center
Other Authors: Hill, Acquilla S.
Format: Government Document Book
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1985.
Series:NASA technical memorandum ; 87600.
Subjects:
Aerofoils > Testing > Statistics.
Aerodynamics, Transonic.
Reynolds number.
Airfoil profiles.
Boeing aircraft.
Cryogenic wind tunnels.
High Reynolds number.
Pressure distribution.
Supercritical airfoils.
Two dimensional bodies.
Wind tunnel models.
Wind tunnel tests.
Online Access:https://purl.fdlp.gov/GPO/LPS85654

Internet

https://purl.fdlp.gov/GPO/LPS85654

Available Online

Holdings details from Available Online
Call Number: NAS 1.15:87600
 
Call Number Status Get It
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Evans: US Documents Microfiche (3rd floor)

Holdings details from Evans: US Documents Microfiche (3rd floor)
Call Number: NAS 1.15:87600
 
Call Number Status Get It
NAS 1.15:87600 Available