NDLI: Airplane wing leading edge variable camber flap

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Airplane wing leading edge variable camber flap

Content Provider	NASA Technical Reports Server (NTRS)
Author	Cole, J. B.
Copyright Year	1980
Description	The invention and design of an aerodynamic high lift device which provided a solution to an aircraft performance problem are described. The performance problem of converting a high speed cruise airfoil into a low speed aerodynamic shape that would provide landing and take-off characteristics superior to those available with contemporary high lift devices are addressed. The need for an improved wing leading edge device that would complement the high lift performance of a triple slotted trailing edge flap is examined. The mechanical and structural aspects of the variable camber flap are discussed and the aerodynamic performance aspects only as they relate to the invention and design of the device are presented.
File Size	759912
Page Count	11
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19800015023
Archival Resource Key	ark:/13960/t47q3ss65
Language	English
Publisher Date	1980-05-01
Access Restriction	Open
Subject Keyword	Aircraft Design, Testing And Performance Aerodynamic Configurations Leading Edge Slats Performance Prediction Airfoils Design Analysis Vibration Tests Aerodynamic Characteristics Camber Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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