Response Surface Modeling of Combined-Cycle Propulsion Components Using Computational Fluid Dynamics.
- Author(s):
- Steffen Jr., C.J.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2002
- Pub. Year:
- 2002
- No.:
- 2002-0542
- Paper no.:
- 2002-0542
- Pages:
- 10
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Inlet Development for a Rocket Based Combined Cycle, Single Stage to Orbit Vehicle Using Computational Fluid Dynamics
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Computational Magnetohydrodynamic Model of a Nonuniform Gasdynamic Mirror Propulsion System
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics
American Institute of Aeronautics and Astronautics |
8
Technical Paper
An investigation of DTNS2D for use as an incompressible turbulence modelling test-bed
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
A Critical Comparison of Several Low Reynolds Number k-ε Turbulencce Models for Flow Over a Backward-Facing Step
National Aeronautics and Space Adminstration |
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
A Computational Magneto Hydrodynamic Model of an Advanced Fusion Fuel Gas Dynamic Mirror Propulsion System.
American Institute of Aeronautics and Astronautics |