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Propulsion System Integration and Test Program (Steady State). Part II. Shared Exit Ejector Nozzle Static Tests
Report Number: AFAPL TR 69-44 Part 02
Author(s): Alfano, David L.
Corporate Author: North American Rockwell Corp Los Angeles CA Los Angeles Div
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 6/1/1969
Pages: 371
Features: + Foldout(s)
Contract: F33615-67-C-1829
Project: None Given
Task: None Given
AD Number: AD0856259
Photo Enhancement: Complete
Abstract Text:
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.
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Cost Effectiveness Study - Bare Base Surfacing Requirements
Report Number: AFAPL TR 69-58
Author(s): Sheets, Mac A.
Corporate Author: Air Force Aero Propulsion Lab Wright-Patterson AFB OH
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 9/1/1969
Pages: 119
Contract: Laboratory Research - No Contract
Project: 8174
Task: 817410
AD Number: AD0864141
Photo Enhancement: Incomplete
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Via National Technical Information Service:
The NTIS Order Number for this report is: AD864141
This report should be available for purchase from NTIS at 1-800-553-NTIS
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Indications of Public Availabilty:
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There has been no verification of an indication of public availability from an inside cover statement
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