Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads /
Saved in:
Author / Creator: | Batina, John T. |
---|---|
Imprint: | Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985. |
Description: | 1 volume. |
Language: | English |
Series: | NASA technical memorandum ; 86320 NASA technical memorandum ; 86320. |
Subject: | |
Format: | E-Resource Microform U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/7243330 |
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 |
Similar Items
-
Analysis of low-speed unsteady airfoil flows /
Published: (2005) -
The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals /
by: Munk, Max M. (Max Michael), 1890-
Published: (1923) -
Airfoil dynamic stall and rotorcraft maneuverability /
by: Bousman, William G.
Published: (2000) -
Tables of properties of airfoil polynomials /
by: Desmarais, Robert N.
Published: (1995) -
Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade /
by: Buffum, Daniel H.
Published: (1996)