Special muffler having 600-ft cross section for reduction of intense noise from burning of jet engine in test section of supersonic wind tunnel at Lewis Flight Propulsion Laboratory in Cleveland.
Noise control for NACA supersonic wind tunnel
Acoustical Soc America -- J
Acoustical Society of America -- Journal ; 27 , n 1
1955
14 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Acoustical treatment for NACA 8- by 6-foot supersonic propulsion wind tunnel
Engineering Index Backfile | 1955
|NACA transonic wind-tunnel test sections
Engineering Index Backfile | 1955
|NACA transonic wind-tunnel test sections
TIBKAT | 1955
|