ANALYSIS OF A JET IN A SUBSONIC CROSSWIND- NASA SYMPOSIUM.
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File Size : 30,5 MB
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Author : Langley Research Center (Hampton, VA)
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Page : 249 pages
File Size : 21,52 MB
Release : 1969
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Page : 260 pages
File Size : 45,56 MB
Release : 1969
Category : Aerodynamics
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Author : National Aeronautics and Space Administration, Scientific and Technical Information Division
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Page : pages
File Size : 24,86 MB
Release : 1969
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Author : United States. National Aeronautics and Space Administration
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Page : 249 pages
File Size : 29,56 MB
Release : 1969
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Page : 249 pages
File Size : 45,70 MB
Release : 1969
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Author : George Kurylowich
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Page : 114 pages
File Size : 24,26 MB
Release : 1979
Category : Helicopters
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Experience as a consultant to the Safety Office at Norton AFB led to compiling the engineering tools presented so that this report can be used by engineering personnel to investigate future incidents/accidents and existing USAF operations that are impacted by the vortical wake hazard. The approach presented is amenable to easy hand computations. Mixed airplane/helicopter operations can be assessed, since the engineering tools to determine the location and strength of the rotor downwash field behind a helicopter are presented. Finally, a simplified mathematical model is given to represent this hazard for use in USAF simulators, to make pilots aware of the problems associated with operating in wake-contaminated airspace.
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Page : 1250 pages
File Size : 29,9 MB
Release : 1970
Category : Government publications
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Author : H. S. Chang
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Page : 174 pages
File Size : 28,56 MB
Release : 1972
Category : Jets
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Page : 704 pages
File Size : 22,61 MB
Release : 1995
Category : Aeronautics
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