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A method for in-flight measurement of ground effect on fixed-wing aircraft.Flight test method for evaluating ground effect on fixed-wing aircraft in which pilot flies at constant angle of attack and power setting during landing approach
Document ID
19670032784
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schweikhard, W.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 66-468
Report Number: AIAA PAPER 66-468
Accession Number
67A11513
Distribution Limits
Public
Copyright
Other
Keywords
FIXED-WING AIRCRAFT
GROUND EFFECT
FLIGHT TEST
IN-FLIGHT MONITORING

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