Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles /

Bibliographic Details

Main Author:	Castner, Raymond S.
Corporate Authors:	NASA Glenn Research Center, Joint Propulsion Conference and Exhibit
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:	NASA technical memorandum ; 216259.
Subjects:	Wind tunnel tests. Supersonic aircraft. Aerodynamic configurations. Low cost. Supersonic wind tunnels. Wind tunnel models. Sonic booms. Static pressure. Pressure sensors. Exhaust nozzles.
Online Access:	https://purl.fdlp.gov/GPO/LPS126598