Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads /

Saved in:
Bibliographic Details
Author / Creator:Batina, John T.
Imprint:Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Description:1 volume.
Series:NASA technical memorandum ; 86320
NASA technical memorandum ; 86320.
Camber (Aerofoils)
Unsteady flow (Aerodynamics)
Aerodynamics, Transonic.
Aerodynamic load.
Aerodynamic configurations.
Computational fluid dynamics.
Transonic flow.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/7243330
Hidden Bibliographic Details
Other authors / contributors:United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Notes:Available via Internet from the NTRS web site. Address as of 07/08/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850010648%5F1985010648.pdf ; current access is available via PURL.
GPO item no.:0830-D (MF)
0830-D (online)
Govt.docs classification:NAS 1.15:86320