Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Clin M. Wang"'
Publikováno v:
AIAA Journal. 33:1447-1453
A new numerical method based on adding a term to the Euler/Navier-Stokes equations has demonstrated that it can effectively treat vortex-dominated flows using low-order numerical schemes and coarse grids. With the technique, numerical diffusion intro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::664c8397451fca6eddf94fa052fad93d
https://doi.org/10.2514/3.12567
https://doi.org/10.2514/3.12567
Publikováno v:
AIAA Journal. 33:289-295
Advanced concepts designed to improve the lift, drag, and pitching moment characteristics of rotor blades have been investigated for the purpose of enhancing rotor maneuver capability. The advantages and disadvantages of these concepts have been eval
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::23efb48053e6998b8777f82d3e4274f5
https://doi.org/10.2514/3.12496
https://doi.org/10.2514/3.12496
Publikováno v:
Computers & Fluids. 22:529-547
Unsteady flow behavior and load characteristics of a 2D VR-7 airfoil with and without a leading-edge slat were studied in the water tunnel of the Aeroflightdynamics Directorate, NASA Ames Research Center. Both airfoils were oscillated sinusoidally be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a0a68883844af222f4a1e37fbd75589
https://doi.org/10.1016/0045-7930(93)90024-4
https://doi.org/10.1016/0045-7930(93)90024-4
Autor:
Paul M. Stremel, Clin M. Wang
Publikováno v:
14th Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d1a93a19ebd2fcf6fc75df9ee96a0d82
https://doi.org/10.2514/6.1996-2490
https://doi.org/10.2514/6.1996-2490
Autor:
Paul M. Stremel, Clin M. Wang
Publikováno v:
34th Aerospace Sciences Meeting and Exhibit.
AIAA 34th Aerospace Sciences Meeting and Exhibit, Reno, NV Jan 15-18, 1996 A new numerical method, vorticity capturing, is used to study wing download. A tilt-rotor wing in hover is modeled with and without an interacting rotor wake. A NACA 0012 airf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1dca7fc897fec51098fde044e8da892f
https://doi.org/10.2514/6.1996-674
https://doi.org/10.2514/6.1996-674
Publikováno v:
33rd Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b2ff6fe41c25544490bc524b8122e906
https://doi.org/10.2514/6.1995-310
https://doi.org/10.2514/6.1995-310
Publikováno v:
11th Computational Fluid Dynamics Conference.
A new numerical method based on adding a term to the Euler/Navier-Stokes equations has been demonstrated it can effectively treat vortex-dominated flows using low-order numerical schemes and coarse grids. The numerical diffusion introduced by convect
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::30fed8b7b45855681cf0b2a9e50b0bb2
https://doi.org/10.2514/6.1993-3343
https://doi.org/10.2514/6.1993-3343