Research Catalog

Title

CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / David O. Davis.

Author

Davis, David O.

Publication

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.

Details

Additional Authors

NASA Glenn Research Center, issuing body.

Description

1 online resource (13 pages) : color illustrations.

Series Statement

NASA/TM ; 2015-218841

Uniform Title

NASA technical memorandum ; 2015-218841.

Alternative Title

Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction

Subject

• Boundary layers
• Computational fluid dynamics
• Shock wave interaction
• Flow measurement
• Turbulent flow

Note

• Title from title screen (viewed on Feb. 2, 2016).
• "September 2015."
• "Prepared for the Joint Fluids Engineering Conference 2015 cosponsored by ASME, JSME, and KSME, Seoul, Korea, July 26-31, 2015

Bibliography (note)

• Includes bibliographical references (page 13).

Call Number

GPO Internet NAS 1.15:2015-218841

OCLC

marcive936387373

Author

Davis, David O., author.

Title

CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / David O. Davis.

Publisher

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2015-218841

NASA technical memorandum ; 2015-218841.

Bibliography

Includes bibliographical references (page 13).

Funding

AJK2015-0634

Connect to:

https://purl.fdlp.gov/GPO/gpo64648

Added Author

NASA Glenn Research Center, issuing body.

Gpo Item No.

0830-D (online)

Sudoc No.

NAS 1.15:2015-218841