Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
An edition of Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control (1999)
By Scott C. Asbury
Publish Date
1999
Publisher
National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor
Language
eng
Pages
-
1-2 of 2 Editions
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
Language: eng
Published In: 1999
Publisher: National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
Language: eng
Published In: 1999
Publisher: National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor