A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool /

Bibliographic Details
Main Authors:	Csank, Jeffrey T. (Author), Stueber, Thomas J. (Author)
Corporate Author:	Joint Propulsion Conference and Exhibit
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
Series:	NASA technical memorandum ; 2012-217714.
Subjects:	Computerized simulation. Propulsion system configurations. Wind tunnel tests. Fuel systems. Propulsion system performance. Turbine engines. Engine inlets.
Online Access:	https://purl.fdlp.gov/GPO/gpo33018

Description
Item Description:	Title from title screen (viewed on Jan. 14, 2013). "September 2012." "Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 30 to August 1, 2012." "AIAA-2012-4149."
Physical Description:	1 online resource (13 pages) : color illustrations.
Bibliography:	Includes bibliographical references (pages 12-13).