Cover Image

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
Description
Item Description:Title from title screen (viewed on Oct. 24, 2011).
"April 2011."
Electronic resource.
Physical Description:1 online resource (65 pages) : illustrations
Bibliography:Includes bibliographical references (pages 26-28).