Open AccessLow and High Speed Propellers for General Aviation — Performance Potential and Recent Wind Tunnel Test Results
Author(s) -
Robert J. Jeracki,
G. A. Mitchell
Publication year - 1981
Publication title -
sae technical papers on cd-rom/sae technical paper series
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.295
H-Index - 107
eISSN - 1083-4958
pISSN - 0148-7191
DOI - 10.4271/811090
Subject(s) - aeronautics , wind tunnel , aviation , aerospace engineering , general aviation , test (biology) , marine engineering , engineering , automotive engineering , computer science , environmental science , geology , paleontology
Research has indicated that there is a significant potential for fuel savings from advanced propellers designed for lower speed general aviation aircraft as well as the advanced turboprop for future Mach 0.6 to 0.8 aircraft. 24 refs.
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