NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Two-dimensional nozzle/airframe integration technology - An overviewThe paper reviews the objectives and some of the accomplishments of a number of programs to develop nonaxisymmetric nozzle technology for future tactical aircraft applications. Specific existing fighter aircraft model tests and preliminary studies are discussed which are designed to generate installed nozzle data, including the effects of thrust vectoring and reversal.
Document ID
19770059121
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Richey, G. K. (USAF, Flight Dynamics Laboratory, Wright-Patterson AFB Ohio, United States)
Berrier, B. L. (NASA Langley Research Center High Speed Aerodynamics Div., Hampton, Va., United States)
Palcza, J. L. (U.S. Naval Air Propulsion Test Center Trenton, N.J., United States)
Date Acquired
August 9, 2013
Publication Date
July 1, 1977
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 77-839
Report Number: AIAA PAPER 77-839
Meeting Information
Meeting: Propulsion Conference
Location: Orlando, FL
Country: US
Start Date: July 11, 1977
End Date: July 13, 1977
Sponsors: American Institute of Aeronautics and Astronautics, Society of Automotive Engineers
Accession Number
77A41973
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

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