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