Cover Image

Slot nozzle effects for reduced sonic boom on a generic supersonic wing section /

Bibliographic Details
Main Author: Castner, Raymond S.
Corporate Authors: NASA Glenn Research Center, AIAA Aerospace Sciences Meeting
Format: Government Document Conference Proceeding eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:NASA technical memorandum ; 216258.
Subjects:
Exhaust nozzles.
Sonic booms.
Wing slots.
Aircraft control.
Computational fluid dynamics.
Exhaust gases.
Supersonic speed.
Mach number.
High aspect ratio.
Online Access:https://purl.fdlp.gov/GPO/LPS126590
Description
Item Description:Title from title screen (viewed on Oct. 7, 2010).
"March 2010."
"AIAA-2010-1386."
Electronic resource.
Physical Description:1 online resource (10 pages) : illustrations
Bibliography:Includes bibliographical references (page 10).