Research on supersonic inlet bleed /
Saved in:
Author / Creator: | Davis, David O. |
---|---|
Imprint: | Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] |
Description: | 1 online resource (24 p.) : ill. (some col.). |
Language: | English |
Series: | NASA/TM ; 2012-217620 NASA technical memorandum ; 2012-217620. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/8951488 |
Other authors / contributors: | Vyas, Manan A. Slater, John W. NASA Glenn Research Center. AIAA Aerospace Sciences Meeting (50th : 2012 : Nashville, Tenn.) |
---|---|
Notes: | Title from title screen (viewed on Dec. 10, 2012). "August 2012." "Prepared for the 50th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Nashville, Tennessee, January 9-12, 2012." "AIAA-2012-0272." Includes bibliographical references (p. 24). Sponsored by National Aeronautics and Space Administration WBS 984754.02.07.03.13.02 E-18208 |
GPO item no.: | 0830-D (online) |
Govt.docs classification: | NAS 1.15:2012-217620 |
Similar Items
-
Analysis of buzz in a supersonic inlet /
by: Chima, Rodrick V.
Published: (2012) -
NASA Glenn 1-by 1-foot supersonic wind tunnel user manual /
Published: (1999) -
Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶ /
by: Loftin, Laurence K.
Published: (1954) -
Mean velocity and turbulence measurements in a 90° curved duct with thin inlet boundary layer : final report /
Published: (1985) -
Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges /
by: Chu, Julio
Published: (1996)