Effects of Flexibility on Aircraft Dynamic Loads and Structural Optimization
- Author(s):
- H. Baluch ( Delft University of Technology, Delft, The Netherlands )
- P. Lisandrin
- R. Slingerland
- M. van Tooren
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-0768
- Paper no.:
- AIAA Paper 2007-768
- Pub. info.:
- Reston, Va: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200702 [CD-ROM 2007 Disc 2]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Design Tradeoffs for Fiber Composite Fuselages Under Dynamic Loads Using Structural Optimization
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Environmental Harm Minimization During Cruise for Preliminary Long-Range Aircraft Design
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Propeller Slipstream Effects on Directional Aircraft Control with One Engine Inoperative
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
A Design & Engineering Engine to Investigate Acoustics in Preliminary Fuselage Design
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Nonlinear Dynamic Response Structural Optimization of a Joined-Wing Using Equivalent Static Loads
American Institute of Aeronautics and Astronautics |