Publikationsdatum:
2019-07-13
Beschreibung:
Hypersonic turbulent boundary layer in adverse pressure gradients studied for transition, measuring static/pitot pressure, stagnation temperature and heat transfer rates
Schlagwort(e):
FLUID MECHANICS
Materialart:
AIAA PAPER 68-44
,
; ADEMIE DES SCIENCES|AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING; Jan 22, 1968 - Jan 24, 1968; NEW YORK, NY
Format:
text
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