Zobrazeno 1 - 10
of 30
pro vyhledávání: '"Stephen J. Alter"'
Autor:
Karl T. Edquist, Stephen J. Alter, Christopher E. Glass, William L. Kleb, Ashley M. Korzun, William A. Wood, Francisco Canabal, Robert Childs, Logan D. Halstrom, Kristen V. Matsuno
Publikováno v:
AIAA SCITECH 2022 Forum.
Autor:
Jeffrey A. Housman, Stephen J. Alter, Ercan Dumlupinar, Bil Kleb, Greg J. Brauckmann, Mihirkumar M. Patel, James R. Koch, Cetin C. Kiris
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
James R. Koch, Ercan Dumlupinar, Jeffrey A. Housman, Cetin C. Kiris, Mihirkumar M. Patel, Bil Kleb, Greg J. Brauckmann, Stephen J. Alter
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
Stephen J. Alter, Greg J. Brauckmann, Matthew N. Rhode, David W. Witte, James C. Ross, Bryan E. Falman, Karl T. Edquist, Thomas K. West, William L. Kleb, Mark Schoenenberger
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
Stephen J. Alter, James C. Ross, Ben Nikaido, Robert Childs, Paul Stremel, Bil Kleb, Scott M. Murman, Joseph A. Garcia, Marie Denison, Thomas K. West, Phil Robinson
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
Paresh Parikh, Veronica Hawke, Kambiz Salari, Matthew N. Rhode, Joseph A. Garcia, Craig A. Hunter, Mihirkumar M. Patel, Stephen J. Alter, Paul Stremel, William L. Kleb, Robert Childs
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
David M. Schuster, William L. Kleb, Christopher E. Glass, Stephen J. Alter, Craig L. Streett, Greg J. Brauckmann
Publikováno v:
33rd AIAA Applied Aerodynamics Conference.
Autor:
Stephen J. Alter, Craig L. Streett, Gregory J. Braukmann, William L. Kleb, Christopher E. Glass, Kelly J. Murphy
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Delayed Detached Eddy Simulation (DDES) predictions of the unsteady transonic flow about a Space Launch System (SLS) configuration were made with the Fully UNstructured Three-Dimensional (FUN3D) flow solver. The computational predictions were validat
Experimental Hypersonic Aerodynamic Characteristics of Mars Surveyor 2001 Precision Lander with Flap
Autor:
Stephen J. Alter, Ramadas K. Prabhu, Tod F. O'Connell, Thomas J. Horvath, F. McNeil Cheatwood
Publikováno v:
Journal of Spacecraft and Rockets. 43:270-281
Aerodynamic wind-tunnel screening tests were conducted on a 0.029-scale model of a proposed Mars Surveyor 2001 Precision Lander (70-deg half-angle spherically blunted cone with a conical afterbody). The primary experimental objective was to determine
Autor:
Stephen J. Alter
Publikováno v:
Journal of Aerospace Computing, Information, and Communication. 3:5-20