A computer based model for the performance analysis of a SCRAMJET propulsion system
Name
20404694-MIT.pdf
Description
Full printable version
Size
4 MB
Format
Adobe PDF
Checksum (MD5)
7ccf8a7a639e39d836ac59d910b9a82b
Author(s)
Ren, Chiang-Hwa
Advisor(s)
Manuel Martinez-Sanchez.
Date Issued
1989
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.
Includes bibliographical references (leaves 73-74).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Persistent DSpace Link
