Cover Image

Mach 10 experimental database of a three-dimensional scramjet inlet flow field /

Bibliographic Details
Main Author: Holland, Scott D.
Corporate Author: Langley Research Center
Format: Government Document Book
Language:English
Published: Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [Available from the National Technical Information Service], [1995]
Series:NASA technical memorandum ; 4648.
Subjects:
Computational fluid dynamics.
Engine inlets.
Flow distribution.
Hypersonic speed.
Inlet flow.
Internal flow.
Laminar boundary layer.
Oblique shock waves.
Pressure measurement.
Shock wave interaction.
Supersonic combustion ramjet engines.
Three dimensional flow.
Wind tunnel tests.
Online Access:https://purl.fdlp.gov/GPO/LPS60779

Internet

https://purl.fdlp.gov/GPO/LPS60779

Evans: US Documents Microfiche (3rd floor)

Holdings details from Evans: US Documents Microfiche (3rd floor)
Call Number: NAS 1.15:4648
 
Call Number Status Get It
NAS 1.15:4648 Available

Available Online

Holdings details from Available Online
Call Number: NAS 1.15:4648
 
Call Number Status Get It
NAS 1.15:4648 Available