Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet /

Bibliographic Details

Main Author:	Maglieri, Domenic J.
Corporate Author:	Langley Research Center
Other Authors:	Henderson, Herbert R., Tinetti, Ana Fiorella, 1962-
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Series:	NASA contractor report ; NASA CR-217150.
Subjects:	F-104 aircraft. Flow distribution. Sonic booms. Supersonic speed. B-70 aircraft. Shock waves. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo14318