Analysis and Design of a Hypersonic Scramjet Engine with a Transition Mach Number of 4.00
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2009 ; Orlando, FL
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 14692-14720
2009-01-01
29 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.