Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Bruce T. Vu"'
Publikováno v:
ASCEND 2021.
Publikováno v:
Earth and Space 2021.
Three-dimensional, Multi-Phase Modeling of a Water Nozzle Injection System Using Adaptive Re-Meshing
Publikováno v:
2018 Fluid Dynamics Conference.
Autor:
James G. Captain, Rupert U. Lee, Ricardo M. Gomez Cano, Jared Berg, Elspeth M. Petersen, Malay Shah, Jon A. Bayliss, Paul E. Hintze, Bruce T. Vu, Alexander Walts, Anthony C. Muscatello, Rene Formoso, Anne J. Meier
Publikováno v:
AIAA SPACE and Astronautics Forum and Exposition.
Here we report further progress in the development of the MARCO POLO-Mars Pathfinder Atmospheric Processing Module (APM). The APM is designed to demonstrate in situ resource utilization (ISRU) of the Martian atmosphere, which primarily consists of ca
Publikováno v:
Scopus-Elsevier
Comparing to conventional CFD methods, meshfree methods have a great potential in dealing with moving boundary problems as mesh points can move in a truly arbitrary manner without the concern of ruining the integrity of the computational mesh. In the
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
This paper describes the use of Smoothed Particle Hydrodynamics (SPH) to simulate the water flow from the rainbird nozzle system used in the sound suppression system during pad abort and nominal launch. The simulations help determine if water from ra
Publikováno v:
The Journal of the Acoustical Society of America. 141:3503-3503
During the study and development of NASA space vehicles, acoustic environments have been a critical design input. This paper surveys some of the key challenges and focuses on the contributions and collaborations of Kenneth J. Plotkin/Wyle Laboratorie
Publikováno v:
44th AIAA Fluid Dynamics Conference.
This paper describes the use of a Volume of Fluid (VOF) multiphase model to simulate the water injected from a rainbird nozzle used in the sound suppression system during launch. The simulations help determine the projectile motion for different wate
Autor:
Christoph Brehm, Bruce T. Vu, Parlier Christopher, Emre Sozer, Cetin C. Kiris, Shayan Moini-Yekta, Michael F. Barad, Jeffrey A. Housman
Publikováno v:
31st AIAA Applied Aerodynamics Conference.
Publikováno v:
21st AIAA Computational Fluid Dynamics Conference.
This paper describes the use of an Eulerian Dispersed Phase (EDP) model to simulate the water injected from the flame deflector and its interaction with supersonic rocket exhaust from a proposed Space Launch System (SLS) vehicle. The Eulerian formula