Analysis of mixing and thrust diagnostics for shock tunnel hot nozzle testing

Analysis of mixing and thrust diagnostics for shock tunnel hot nozzle testing

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.

Bibliographic Details
Main Author: Creviston, Douglas Orie, 1975-
Other Authors: Ian A. Waitz.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2009
Subjects:
Aeronautics and Astronautics
Online Access:http://hdl.handle.net/1721.1/50074

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