Rocket-based combined cycle engine technology development : inlet CFD validation and application /

Saved in:
Bibliographic Details
Author / Creator:DeBonis, James R., author.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996.
Description:1 online resource (18 pages) : illustrations.
Language:English
Series:NASA technical memorandum ; 107274
NASA technical memorandum ; 107274.
Subject:Rocket engine design.
Rocket engines.
Engine inlets.
Navier-Stokes equation.
Computational fluid dynamics.
Jet engines -- Air intakes.
Rocket engines.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10910425
Hidden Bibliographic Details
Varying Form of Title:Inlet computational fluid dynamics validation and application
Other authors / contributors:Yungster, Shaye, author.
Lewis Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Notes:Title from title screen (viewed July 19, 2016).
"June 1996"--Report documentation page.
"Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996."
"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
"ICOMP-96-6."
"AIAA-96-3145."
Includes bibliographical references (pages 7-8).
Sponsored by the National Aeronautics and Space Administration WU-505-70-62 E-10342
Other form:Print version: DeBonis, James R. Rocket-based combined cycle engine technology development
Microfiche version: DeBonis, James R. Rocket-based combined cycle engine technology development
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:107274