Aeroacoustic measurement and analysis of transient supersonic hot nozzle flows

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999. === Includes bibliographical references (p. 195-199). === A transient testing technique for the study of jet noise was investigated and assessed. A shock tunnel facility was utilized to produce short d...

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Bibliographic Details
Main Author: Kirk, Daniel Robert, 1975-
Other Authors: Ian A. Waitz.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2006
Subjects:
Online Access:http://hdl.handle.net/1721.1/29883