Accession Number : AD0839562
Title : PROCEDURES AND SUGGESTED PROGRAMMING EMPHASIS TO OBTAIN CRITERIA ESSENTIAL TO ATTAINING PROPULSION SYSTEM FLOW STABILITY.
Descriptive Note : Rept. for Mar 65-Dec 67,
Corporate Author : AIR FORCE AERO PROPULSION LAB WRIGHT-PATTERSON AFB OH
Personal Author(s) : Gratz, Harlan J.
Report Date : MAY 1968
Pagination or Media Count : 31
Abstract : An approach is made to develop a planning concept for establishing the proper compromise between propulsion-system flow stability and performance. Testing is considered to be a tool for predicting flow compatibility and lead-time funding requirements. The types of compromise studies to be accomplished prior to the Contract Definition Phase are stressed. The use of this planning tool will organize the results of the compromise studies to permit the selection of an airframe-engine combination at the system acquisition phase; statistically, this selection will represent the most compatible system. (Author)
Descriptors : *TURBOJET INLETS), (*JET ENGINES, (*JET ENGINE INLETS, AERODYNAMIC CHARACTERISTICS), TURBOJET ENGINES, TURBOFAN ENGINES, STABILITY, AIRCRAFT ENGINES, PERFORMANCE(ENGINEERING), JET FIGHTERS, AIRFRAMES, STANDARDS, JET PROPULSION.
Subject Categories : Fluid Mechanics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE