NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Study of an engine flow diverter system for a large scale ejector powered aircraft modelRequirements were established for a conceptual design study to analyze and design an engine flow diverter system and to include accommodations for an ejector system in an existing 3/4 scale fighter model equipped with YJ-79 engines. Model constraints were identified and cost-effective limited modification was proposed to accept the ejectors, ducting and flow diverter valves. Complete system performance was calculated and a versatile computer program capable of analyzing any ejector system was developed.
Document ID
19810019558
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Springer, R. J. (General Dynamics Corp. Fort Worth, TX, United States)
Langley, B. (General Dynamics Corp. Fort Worth, TX, United States)
Plant, T. (General Dynamics Corp. Fort Worth, TX, United States)
Hunter, L. (General Dynamics Corp. Fort Worth, TX, United States)
Brock, O. (General Dynamics Corp. Fort Worth, TX, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-166163
Accession Number
81N28096
Funding Number(s)
CONTRACT_GRANT: NAS2-10680
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available