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DEVELOPMENT OF A STALL IMPROVEMENT PACKAGE FOR THE GULFSTREAM IV GULFSTREAM AEROSPACE CORPORATION Savannah, Georgia

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Bruner, Hugh S., author.
Conference Name:
General Aviation Aircraft Meeting and Exposition (1989-04-11 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1989
Summary:
A package of aerodynamic devices have been developed for the Gulfstream IV to enhance its stall characteristics. This package consists of an array of small vortilons beneath the leading edge plus a small stall strip inboard. This package has allowed Gulfstream to tailor the pre- and post-stall characteristics without compromising the wing's excellent transonic cruise characteristics. A discussion of the background that prompted this investigation is presented, the mechanisms through which the package work are explained and a brief review of the flight test program is given. As a conclusion, a comparison of the before and after characteristics are shown
Notes:
Vendor supplied data
Publisher Number:
891021
Access Restriction:
Restricted for use by site license

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