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by H. Andrew Chuang
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The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel
Norbert Ulbrich
Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
Wendy B. Lessard
Implementation of a two-equation K-[omega] turbulence model in NPARC
Dennis A. Yoder
Higher-order approximations in interactive airfoil calculations
D. W. Zingg
Description of panel method code ANTARES
An extended Lagrangian method
Meng-Sing Liou
Doppler global velocimetry at NASA Glenn Research Center
Christian T. Lant
Wing pressure distributions from subsonic tests of a high-wing transport model
Zachary T. Applin
Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report
Joseph R. Hauser
M. S. Liou