Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Shreekant Agrawal"'
Autor:
Shreekant Agrawal, Pichuraman Sundaram
Publikováno v:
AIAA Aviation 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::247089428a761d36ca45d36d469d5ed6
https://doi.org/10.2514/6.2019-3609
https://doi.org/10.2514/6.2019-3609
Autor:
David W. Levy, Thomas Zickuhr, John Vassberg, Shreekant Agrawal, Richard A. Wahls, Shahyar Pirzadeh, Michael J. Hemsch
Publikováno v:
Journal of Aircraft. 40:875-882
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dfee3a4e787a1a995afcf97fa462352b
https://doi.org/10.2514/2.6877
https://doi.org/10.2514/2.6877
Publikováno v:
Journal of Aircraft. 28:721-727
An analysis of the boundary layer and its stability with and without suction on a supersonic cruise fighter wing configuration is presented for a freestream Mach number of 2.0 and an angle of attack of 4.0 deg. The inviscid pressures obtained from an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::552b185634609b3488e183224c2ffd58
https://doi.org/10.2514/3.46088
https://doi.org/10.2514/3.46088
Thesis(M.S.)--Auburn University, 2006.
Vita. Includes bibliographic references (p.74-78).
Vita. Includes bibliographic references (p.74-78).
Autor:
David W. Levy, Tom Zickuhr, John Vassberg, Shreekant Agrawal, Richard A. Wahls, Shahyar Pirzadeh, Michael J. Hemsch
Publikováno v:
Journal of Aircraft. 40
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f64817e962586d00523304de7296ccb7
https://doi.org/10.2514/1.1684
https://doi.org/10.2514/1.1684
Publikováno v:
8th Symposium on Multidisciplinary Analysis and Optimization.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0cbea655d790c00b1829a1c849b12124
https://doi.org/10.2514/6.2000-4733
https://doi.org/10.2514/6.2000-4733
Autor:
Shreekant Agrawal, Robert P. Narducci
Publikováno v:
38th Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::be83ac39654d2f6d1cfe5760feafaf27
https://doi.org/10.2514/6.2000-382
https://doi.org/10.2514/6.2000-382
Autor:
Peter Hartwich, Shreekant Agrawal
Publikováno v:
13th Computational Fluid Dynamics Conference.
A highly automated method is presented for rapidly adjusting multiblock patched grids over complex configurations during aerodynamic shape optimization or aeroelastic analyses. A very low level of user-intervention is achieved by making the block bou
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2bbe241b9804172d4e13eba5c3dd707d
https://doi.org/10.2514/6.1997-2038
https://doi.org/10.2514/6.1997-2038
Autor:
Shreekant Agrawal, Peter Hartwich
Publikováno v:
14th Applied Aerodynamics Conference.
In an attempt to reduce the expenditure associated with aerodynamic shape optimization, the suitability of orthonormal functions for an efficient, accurate, and user-independent parametrization of twoand three-dimensional aerodynamic shapes is explor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0156e41255a4cab08b46fa9e8e3b42fd
https://doi.org/10.2514/6.1996-2419
https://doi.org/10.2514/6.1996-2419
Publikováno v:
10th Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c57725fe7567e81d1887f0e884e97fbd
https://doi.org/10.2514/6.1992-2654
https://doi.org/10.2514/6.1992-2654