Accession Number : AD0858287
Title : F-84F Engine Air Inlet Ground Protective Screen Test.
Descriptive Note : Technical note,
Corporate Author : WRIGHT AIR DEVELOPMENT CENTER WRIGHT-PATTERSON AFB OH
Personal Author(s) : Brown, William E.
Report Date : 06 AUG 1954
Pagination or Media Count : 10
Abstract : Static engine runs of F-84F aircraft were accomplished with and without a ground protective screen installed over the engine air inlet duct. It was determined that use of this screen did not cause the exhaust gas temperature or the inlet duct differential pressures to exceed prescribed limits.
Descriptors : (*JET ENGINES, TURBOJET INLET SCREENS), AIR FILTERS, TURBOJET INLETS, DUCT INLETS, PRESSURE, TEMPERATURE, EXHAUST GASES, CAPTIVE TESTS, ACCEPTABILITY, PRESSURE GAGES.
Subject Categories : Aircraft
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE