An investigation into the use of an existing shock tube as a driver for a hypersonic shock tunnel
Contributors: Shreeve, Raymond P.
Publisher: Naval Postgraduate School; Available from the National Technical Information Service
Published: 1989
Place of publication: Monterey, Calif; Springfield, Va
Language: eng
Number of pages: 139
Notes: Thesis advisor, Raymond P. Shreeve.

ADA208483.

Thesis (M.S. in A.E.) Naval Postgraduate School, Mar. 1989.

Includes bibliographical references.