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Numerical simulation of a powered-lift landingThe flow field about a delta wing equipped with thrust reverse jets in slow speed flight near the ground has been computed. Results include the prediction of the flow about the delta wing at four fixed heights above the ground, and simulated landing, in which the delta wing descends towards the ground. Comparison of computed and experimental lift coefficients indicates that the simulations can capture at least the qualitative trends in lift-loss encountered by thrust-vectoring aircraft operating in ground effect.
Document ID
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Chawla, Kalpana
(MCAT Inst. Moffett Field, CA., United States)
Vandalsem, William R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 16, 2013
Publication Date
November 1, 1993
Publication Information
Publication: AGARD, Computational and Experimental Assessment of Jets in Cross Flow
Subject Category
Aircraft Design, Testing And Performance
Accession Number
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