Propulsion System Integration and Test Program (Steady State). Part II. Shared Exit Ejector Nozzle Static Tests

Item

Title
Propulsion System Integration and Test Program (Steady State). Part II. Shared Exit Ejector Nozzle Static Tests
Date
1969
Index Abstract
Coming Soon
Photo Quality
Complete
Report Number
AFAPL TR 69-44 Part 02
Corporate Author
North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory
Air Force Aero Propulsion Laboratory
Extent
371
NTRL Accession Number
AD856259
Identifier
AD0856259
Access Rights
Export Control
Distribution Classification
1
Contract
F33615-67-C-1829
DoD Project
None Given
DoD Task
None Given
DTIC Record Exists
No
Distribution Change Authority Correspondence
AFAPL LTR
Date Modified
Scanned by request 3/21/2007 submitted by a Private Citizen (No Known Affiliation)
Abstract
A program for designing and conducting tests on a shared exit ejector nozzle was formulated to provide experimental verification of available analytic techniques, where applicable, and to provide data at those conditions where analytic techniques were not applicable so that this nozzle concept could be evaluated. The test plan was formulated around the complete spectrum of engine cycle data for an Integrated Propulsion System Tactical Fighter. Results from this test program indicate that the reliability of the available analytic techniques for predicting nozzle performance is dependent on an accurate estimate of the internal losses and aerodynamic flow areas involved.
Report Availability
Full text available
Date Issued
1969-06
Publisher
Wright-Patterson Air Force Base, OH : Air Force Aero Propulsion Laboratory, Air Force Systems Command
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource
Creator
Alfano, David L.
Media
AFAPLTR69-044part02.pdf

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