Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle
By: Scott C. Asbury and Craig A. Hunter.
Contributors: Hunter, Craig A.; Langley Research Center.; United States. National Aeronautics and Space Administration.
Series: NASA/TP -- 1999-209093.; NASA technical paper -- 209093.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Convergent-divergent nozzles.; Boundary layer separation.; Wind tunnel nozzles.; Wind tunnel tests.; Nozzle flow.; Oblique shock waves.; Flow visualization.
Notes: Shipping list no.: 99-0723-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.