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Estimation of wing nonlinear aerodynamic characteristics at supersonic speedsA computational system for estimation of nonlinear aerodynamic characteristics of wings at supersonic speeds was developed and was incorporated in a computer program. This corrected linearized theory method accounts for nonlinearities in the variation of basic pressure loadings with local surface slopes, predicts the degree of attainment of theoretical leading edge thrust, and provides an estimate of detached leading edge vortex loadings that result when the theoretical thrust forces are not fully realized.
Document ID
19810001496
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Carlson, H. W. (NASA Langley Research Center Hampton, VA, United States)
Mack, R. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NASA-TP-1718
L-13589
Accession Number
81N10004
Funding Number(s)
PROJECT: RTOP 505-31-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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