Publication Date:
2019-07-13
Description:
Aerodynamic performance characteristics of three entry vehicles designed for maximum L/D ratio of three and two at Mach 19 and Reynolds number 3,200,000 tested in 22-inch Langley helium tunnel
Keywords:
AERODYNAMICS
Type:
AIAA PAPER 67-138
,
AEROSPACE SCIENCES MEETING; Jan 23, 1967 - Jan 26, 1967; NEW YORK, NY
Format:
text
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