NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Integration of ejectors into high-speed aircraftThe integration of ejectors into forebodies is considered for transonic and supersonic flight. Topics discussed include mixing flow in ducts, prediction of flow fields and external aerodynamics.
Document ID
19800001880
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Duvvuri, T. (Duvvuri Research Associates Chula Vista, CA, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: NASA. Ames Res. Center Workshop on Thrust Augmenting Ejectors
Subject Category
Aerodynamics
Accession Number
80N10119
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19800001868Collected WorksWorkshop on Thrust Augmenting Ejectors
No Preview Available