An Optimization-Based Approach to Injector Element Design
- Author(s):
- Tucker, P. Kevin ( NASA Marshall Space Flight Center )
- Shyy, Wei
- Vaidyanathan, Rajkumar
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 2000
- Pub. Year:
- 2000
- No.:
- 2000-3220
- Paper no.:
- 00-3220
- Page(from):
- 1
- Page(to):
- 13
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Response Surface and Neural Network Techniques for Rocket Engine Injector Optimization
American Institute of Aeronautics and Astronautics |
7
Technical Paper
An Approach to Improved Credibility of CFD Calculations for Rocket Injector Design
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Response surface and neural network techniques for rocket engine injector optimization
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Response Surface Approximation of Pareto Optimal Front in Multi-objective Optimization
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Global Sensitivity and Trade-Off Analyses for Multi-Objective Liquid Rocket Injector Design
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Aerothermodynamic Optimization of Hypersonic Vehicle TPS Design by POD/RSM-Based Approach
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |