Reduced-Order Stability Analysis Model for Predicting Dynamic Instabilities
- Author(s):
- S. Rani ( CFD Research Corporation, Huntsville, AL )
- C. Smith
- T. Lieuwen ( Georgia Institute of Technology, Atlanta, GA )
- S. Hemchandra
- B. Sekar ( Air Force Research Laboratory, WPAFB, OH )
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-5649
- Paper no.:
- AIAA Paper 2007-5649
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200717 [CD-ROM 2007 Disc 17]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
CFD Predictions of Damköhler Number Fields for Reduced Order Modeling of V-Gutter Flame Stability
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Using Fourth Order Accurate Spatial Integration on Unstructured Meshes to Reduce LES Run Times
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Residualization of an Aircraft Aeroelastic Reduced Order Model to Obtain Static Stability Derivatives
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Reduced Run Times for Pressure-Based, Large Eddy Simulations Using Fourth Order, Implicit Time Integration
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
4
Technical Paper
Active control analysis for combustion-driven dynamic instabilities in gas-turbine combustors
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
A Volterra Kernel Reduced-Order Model Approach for Nonlinear Aeroelastic Analysis
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Studies of Active Instability Control Effectiveness in a High Pressure, Liquid Fueled Combustor
American Institute of Aeronautics and Astronautics |