The gas turbine requirements for V/STOL aircraft are strongly influenced by the type of airplane and the mission to be performed. For pusposes of this paper, the gas turbine requirements are established in several propulsion-system concepts which encompass the majority of engine requirements necessary to the V/STOL airplanes. General requirements are explored which are common to gas turbines regardless of mission or airplane type. Specific requirements for the air-superiority fighter airplane, the subsonic fighter attack airplane, and the transport-cargo type of airplane are discussed. These three types of airplanes are propelled by propulsion systems incorporating lift turbojet engines, turbofan engines, fans with remote gas generators, and turboprop engines.
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ASME 1967 Gas Turbine Conference and Products Show
March 5–9, 1967
Houston, Texas, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7988-7
PROCEEDINGS PAPER
V/STOL Aircraft Gas Turbine Requirements Free
O. G. Robbins
O. G. Robbins
LTV Aerospace Corporation, Dallas, TX
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O. G. Robbins
LTV Aerospace Corporation, Dallas, TX
Paper No:
67-GT-48, V001T01A047; 12 pages
Published Online:
April 28, 2015
Citation
Robbins, OG. "V/STOL Aircraft Gas Turbine Requirements." Proceedings of the ASME 1967 Gas Turbine Conference and Products Show. ASME 1967 Gas Turbine Conference and Products Show. Houston, Texas, USA. March 5–9, 1967. V001T01A047. ASME. https://doi.org/10.1115/67-GT-48
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