NASA Logo, External Link
Facebook icon, External Link to NASA STI page on Facebook Twitter icon, External Link to NASA STI on Twitter YouTube icon, External Link to NASA STI Channel on YouTube RSS icon, External Link to New NASA STI RSS Feed AddThis share icon
 

Record Details

Record 36 of 6623
Hypersonic propulsion
External Online Source: doi:10.1016/0360-1285(89)90008-7
Author and Affiliation:
Cheng, SIN-I.(Princeton University, NJ, United States)
Abstract: The paper reviews the whys and hows of the concept of supersonic combustion for hypersonic propulsion. Attention is given to the problem areas, the current research and development efforts, and their implications. The operating boundary of the SCRAMJET is reasonably well defined. The paper also explores some air-breathing alternatives that may go beyond SCRAMJETS.
Publication Date: Jan 01, 1989
Document ID:
19900034894
(Acquired Nov 28, 1995)
Accession Number: 90A21949
Subject Category: AIRCRAFT PROPULSION AND POWER
Document Type: Journal Article
Publication Information: Progress in Energy and Combustion Science; (ISSN 0360-1285); 15; 3, 19
Publisher Information: United Kingdom
Contract/Grant/Task Num: NAS1-17234
Financial Sponsor: NASA; United States
Organization Source: Princeton Univ.; NJ, United States
Description: 20p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: Copyright
NASA Terms: AIRSPEED; HYPERSONIC AIRCRAFT; HYPERSONIC FLOW; JET PROPULSION; SUPERSONIC COMBUSTION RAMJET ENGINES; GAS MIXTURES; MACH NUMBER; TURBULENT FLOW
Imprint And Other Notes: Progress in Energy and Combustion Science (ISSN 0360-1285), vol. 15, no. 3, 1989, p. 183-202.
Availability Source: Other Sources
› Back to Top
Find Similar Records
NASA Logo, External Link
NASA Official: Gerald Steeman
Site Curator: STI Program
Last Modified: August 18, 2011
Contact Us