Accession Number:

ADA067063

Title:

Investigation of Transition of Laminar Boundary Layer into Turbulent in Hypersonic Impulse Tunnel IT-301 at M = 8-11.5,

Personal Author(s):

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1978-08-11

Supplementary Note:

Edited trans. of Aerofizicheskiye Issledovaniya Institut Teoreticheskoy i Prikladnoy Mekhaniki SO AN USSR n2 p89 1973, by Robert A. Potts.

Pages:

0008

Descriptors:

Subject Categories:

Modernization Areas:

File Size:

3.18MB

View The Document