-
1
-
-
85086615377
-
A shape optimization methodology for reducing the sonic boom initial pressure rise
-
AIAA paper 02-0145, Reno, NV, January
-
B. Argrow C. Farhat, K. Maute and M. Nikbay. A shape optimization methodology for reducing the sonic boom initial pressure rise. AIAA paper 02-0145, AIAA 40th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2002.
-
(2002)
AIAA 40th Aerospace Sciences Meeting and Exhibit
-
-
Argrow, B.1
Farhat, C.2
Maute, K.3
Nikbay, M.4
-
2
-
-
34250808918
-
Sonic boom alleviation using keel configurations
-
AIAA paper 02-0149, Reno, NV, January
-
M. Orr J. Mozingo F. Marconi, R. Bowersox and J. Schetz. Sonic boom alleviation using keel configurations. AIAA paper 02-0149, AIAA 40th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2002.
-
(2002)
AIAA 40th Aerospace Sciences Meeting and Exhibit
-
-
Orr, M.1
Mozingo, J.2
Marconi, F.3
Bowersox, R.4
Schetz, J.5
-
3
-
-
0003655741
-
Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes
-
AIAA Paper 81-1259, January
-
A. Jameson, W. Schmidt, and E. Turkel. Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes. AIAA Paper 81-1259, January 1981.
-
(1981)
-
-
Jameson, A.1
Schmidt, W.2
Turkel, E.3
-
4
-
-
0005914380
-
Studies of alternative numerical optimization methods applied to the brachistochrone problem
-
A. Jameson and J. C. Vassberg. Studies of alternative numerical optimization methods applied to the brachistochrone problem. OptiCON 99, 1999.
-
(1999)
OptiCON
, vol.99
-
-
Jameson, A.1
Vassberg, J.C.2
-
5
-
-
34250896661
-
Development of a quiet supersonic aircraft with technology applications to military and civil aircraft
-
AIAA paper 02-0519, Reno, NV, January
-
S. Komadina, A. Drake, and S. Bruner. Development of a quiet supersonic aircraft with technology applications to military and civil aircraft. AIAA paper 02-0519, AIAA 40th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2002.
-
(2002)
AIAA 40th Aerospace Sciences Meeting and Exhibit
-
-
Komadina, S.1
Drake, A.2
Bruner, S.3
-
6
-
-
85088722268
-
A comparison of the continuous and discrete adjoint approach to automatic aerodynamic optimization
-
AIAA paper 2000-0667, Reno, Nevada, January
-
S. Nadarajah and A. Jameson. A comparison of the continuous and discrete adjoint approach to automatic aerodynamic optimization. AIAA paper 2000-0667, 38th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 2000.
-
(2000)
38th Aerospace Sciences Meeting and Exhibit
-
-
Nadarajah, S.1
Jameson, A.2
-
7
-
-
85088757540
-
Studies of the continuous and discrete adjoint approaches to viscous automatic aerodynamic shape optimization
-
AIAA paper 2001-2530, Anaheim, CA, June
-
S. Nadarajah and A. Jameson. Studies of the continuous and discrete adjoint approaches to viscous automatic aerodynamic shape optimization. AIAA paper 2001-2530, 15th. Computational Fluid Dynamics Conference, Anaheim, CA, June 2001.
-
(2001)
15th. Computational Fluid Dynamics Conference
-
-
Nadarajah, S.1
Jameson, A.2
-
8
-
-
33746874248
-
An adjoint method for the calculation of non-collocated sensitivities in supersonic flow
-
Cambridge, MA, June
-
S. Nadarajah, A. Jameson, and J. J. Alonso. An adjoint method for the calculation of non-collocated sensitivities in supersonic flow. In Proceedings of First MIT Conference on Computational Fluid and Solid Mechanics, Cambridge, MA, June 2001.
-
(2001)
Proceedings of First MIT Conference on Computational Fluid and Solid Mechanics
-
-
Nadarajah, S.1
Jameson, A.2
Alonso, J.J.3
-
9
-
-
34250861159
-
-
S. Nadarajah, A. Jameson, and J. J. Alonso. An adjoint method for the calculation of remote sensitivities in supersonic flow. AIAA Paper 2002-0261, 40th. Aerospace Sciences Meething and Exhibit, Reno, NV, Jan 2002.
-
S. Nadarajah, A. Jameson, and J. J. Alonso. An adjoint method for the calculation of remote sensitivities in supersonic flow. AIAA Paper 2002-0261, 40th. Aerospace Sciences Meething and Exhibit, Reno, NV, Jan 2002.
-
-
-
|