Zobrazeno 1 - 10
of 26
pro vyhledávání: '"Alaa A. Elmiligui"'
Publikováno v:
Journal of Aircraft. 58:781-792
A wind tunnel test was performed in the 0.3-Meter Cryogenic Transonic Tunnel at the NASA Langley Research Center to investigate the impact of various boundary layer thickeners on the height and sha...
Publikováno v:
Journal of Aircraft. 56:928-937
The NASA Tetrahedral Unstructured Software System with the USM3D flow solver was used to compute the test cases for the Second AIAA Sonic Boom Prediction Workshop (SBPW2). The intent of this paper ...
Autor:
Gaetan K. Kenway, William E. Milholen, Michael D. Bozeman, Christopher J. Cramer, Gregory S. Jones, Alaa A. Elmiligui, Christopher M. Cagle
Publikováno v:
AIAA Scitech 2020 Forum.
Publikováno v:
AIAA Scitech 2020 Forum.
A wind tunnel test was performed in the 0.3-Meter Cryogenic Transonic Tunnel at the NASA Langley Research Center to investigate the impact of various boundary layer thickeners on the height and shape of the boundary layer on the aft portion of a semi
Publikováno v:
Journal of Aircraft. 54:417-427
Numerical simulations of flow around the F-16XL are presented as a contribution to the Cranked Arrow Wing Aerodynamics Project International II. The NASA Tetrahedral Unstructured Software System with its USM3D solver is used to perform numerical simu
Publikováno v:
35th AIAA Applied Aerodynamics Conference.
Autor:
Susan E. Cliff, Derek J. Dalle, Marie Denison, Nathanial T. Smith, Courtney S. Winski, Donald A. Durston, Brennan T. Blumenthal, Raymond S. Castner, Alaa A. Elmiligui, Melissa B. Carter, Patrick R. Shea
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Publikováno v:
Journal of Aircraft. 50:778-790
A tetrahedral mesh generation method for acquiring accurate sonic boom pressure signatures several body lengths from an aircraft model has been developed. The method serves as a tool for aerodynamicists to efficiently create useful meshes for sonic b
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
The NASA Advanced Air Vehicles Program, Commercial Supersonics Technology Project seeks to advance tools and techniques to make over-land supersonic flight feasible. In this study, preliminary computational results are presented for future tests in t
Autor:
Walter E. Bruce, Melissa B. Carter, Alaa A. Elmiligui, Courtney S. Winski, Sudheer Nayani, Raymond S. Castner
Publikováno v:
54th AIAA Aerospace Sciences Meeting.