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INLET PROTECTION FOR AIRCRAFT GAS TURBINE ENGINES
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English
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Citation
LITTON, R., "INLET PROTECTION FOR AIRCRAFT GAS TURBINE ENGINES," SAE Technical Paper 540085, 1954, https://doi.org/10.4271/540085.Also In
References
- Memorandum Report MCREXP-44 DeRemer J. E. Engineering Division, Air Materiel Command 10 August 1848 “Necessity and Use of Air Inlet Protective Screens in USAF Gas Turbine Powered Aircraft”
- Technical Note WCLP-53-41 Smith D. A. USAF Power Plant Laboratory, Wright Air Development Center 10 February 1953 “Necessity of Retractable Air Inlet Screens in Axial-Flow Turbojet Engine Powered Aircraft”
- Technical Note WCLP-53-89 Smith D. A. USAF Power Plant Laboratory, Wright Air Development Center 2 April 1953 “Object Retention Properties of Retractable Air Inlet Screens”
- Technical Note WCLP-52-83 Lindell Keith USAF Power Plant Laboratory, Wright Air Development Center 29 October 1952 “Foreign Object Damage Tests - J35 Turbojet Engines”
- Memorandum Report WCNE-526-1 Spencer H. E. Equipment Laboratory, Wright Air Development Center 24 September 1951 “Screen Protective, Jet Aircraft, Intake Duct, Ground”
- Memorandum Report WCNE-526-8 Litton R. S. Power Plant Laboratory, Wright Air Development Center 19 May 1952 “Retractable Inlet Screens for Gas Turbine Engines”
- Memorandum Report MCREXP-44 Haaser Walter L. Engineering Division, Air Materiel Command 25 November 1949 “Foreign Articles Retained by Jet Engine Fixed Inlet Screen During a Service Test”