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Development of spin resistance criteria for light general aviation airplanesA brief history of stall/spin technology for light general aviation airplanes is presented. Criteria needed to describe desirable characteristics of a spin-resistant airplane and means to evaluate airplanes for compliance with the criteria have been developed. Initial results from limited flight tests of an experimental high-wing airplane indicated that the basic configuration would not meet the spin resistance criteria. Further tests with the airplane modified to enhance its spin resistance are planned.
Document ID
19860047401
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dicarlo, D. J. (NASA Langley Research Center Hampton, VA, United States)
Stough, H. P., III (NASA Langley Research Center Hampton, VA, United States)
Glover, K. E. (NASA Langley Research Center Hampton, VA, United States)
Brown, P. W. (NASA Langley Research Center Hampton, VA, United States)
Patton, J. M., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1986
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 86-9812
Report Number: AIAA PAPER 86-9812
Accession Number
86A32139
Distribution Limits
Public
Copyright
Other

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