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FLIGHT TEST RESULTS FOR AN ADVANCED TECHNOLOGY LIGHT AIRPLANE WING

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Kohlman, David L., author.
Conference Name:
National Business Aircraft Meeting and Engineering Display (1974-04-02 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1974
Summary:
Flight test results are reported for a Cessna Cardinal single engine light airplane modified by the installation of advanced technology wings incorporating reduced area, Fowler and Kruger flaps, and spoilers for roll and flight path control. Comparisons with the unmodified airplane show increased cruise speeds, smoother ride in turbulence, and major increases in maximum lift coefficient. Excellent roll control is achieved with spoilers. Several design features incorporated in the new wings show considerable promise for incorporation in future light airplanes
Notes:
Vendor supplied data
Publisher Number:
740368
Access Restriction:
Restricted for use by site license

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