Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air
By: William L. Wells.
Contributors: Langley Research Center
Publisher: Langley Research Center
Published: 1990
Place of publication: Hampton, Va
Number of pages: 55
Subjects: Aeroassist Flight Experiment; Hypersonic flow; Hypersonic wakes
Notes: Includes bibliographical references: p. 9-10.