Effect of protuberance shape and orientation on Space Shuttle Orbiter boundary-layer transition /

Bibliographic Details

Main Author:	King, Rudolph A.
Corporate Author:	Langley Research Center
Other Authors:	Berry Scott A., Kegerise, Michael A.
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2008]
Series:	NASA technical memorandum ; 215103.
Subjects:	Boundary layer transition. Hypersonics. Protuberances. Space shuttle orbiters. Thermography. Shapes. Heat transfer.
Online Access:	https://purl.fdlp.gov/GPO/LPS126582