Experimental and computational sonic boom assessment of Boeing N+2 low boom models /

Bibliographic Details

Main Author:	Durston, D. A. (Author)
Format:	Government Document eBook
Language:	English
Published:	Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, February 2015.
Series:	NASA technical paper ; 2015-218482.
Subjects:	Computational fluid dynamics. Pressure measurement. Sonic booms. Supersonic test apparatus. Supersonic wind tunnels.
Online Access:	https://purl.fdlp.gov/GPO/gpo57237 http://purl.fdlp.gov/GPO/gpo57237