

#WING AND AIRFOLIL GEOMETRY X 21 CODE#
Emulsion on film diazo Extent 1 volume Form of item microfiche Generation first generation master Media category microform Media MARC source rdamedia Media type code Distributed to depository libraries in microficheĬarrier category microfiche Carrier category codeĬarrier MARC source rdacarrier Color black and white Content category text Content type codeĬontent type MARC source rdacontent Control code 26603574 Dimensions 4圆 in.Washington, DC, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, Springfield, Va., For sale by the National Technical Information Service, 1992.Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds.Label Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds, Richard M.
#WING AND AIRFOLIL GEOMETRY X 21 SERIES#
Series statement NASA technical paper Series volume 3105

Wesselmann National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program For sale by the National Technical Information Service] : [Springfield, Va 1992 Australian/Harvard Citation Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds / Richard M. Wood, Richard M. and Byrd, James E. and Wesselmann, Gary F. and United States.

Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds.
