NDLI: A study of prediction methods for the high angle-of-attack aerodynamics of straight wings and fighter aircraft

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A study of prediction methods for the high angle-of-attack aerodynamics of straight wings and fighter aircraft

Content Provider	NASA Technical Reports Server (NTRS)
Author	Mendenhall, M. R. Perkins Jr., S. C. McMillan, O. J.
Copyright Year	1984
Description	Work is described dealing with two areas which are dominated by the nonlinear effects of vortex flows. The first area concerns the stall/spin characteristics of a general aviation wing with a modified leading edge. The second area concerns the high-angle-of-attack characteristics of high performance military aircraft. For each area, the governing phenomena are described as identified with the aid of existing experimental data. Existing analytical methods are reviewed, and the most promising method for each area used to perform some preliminary calculations. Based on these results, the strengths and weaknesses of the methods are defined, and research programs recommended to improve the methods as a result of better understanding of the flow mechanisms involved.
File Size	5921643
Page Count	203
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19840009063
Archival Resource Key	ark:/13960/t3gx9504p
Language	English
Publisher Date	1984-01-01
Access Restriction	Open
Subject Keyword	Aerodynamics Aerodynamic Configurations Subsonic Flow Rectangular Wings Nonlinearity Angle of Attack General Aviation Aircraft Fighter Aircraft Prediction Analysis Techniques Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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