In-flight Output Only Modal Analysis of Aircraft Structural Dynamics.
- Author(s):
- Publication title:
- 2008 SAE Noise and Vibration Conference and Exhibition : technical paper
- Title of ser.:
- Society of Automotive Engineers technical paper series
- Ser. no.:
- 2008
- Pub. Year:
- 2008
- No.:
- 2008-36-0536
- Paper no.:
- 2008-36-0536
- Pages:
- 8
- Pub. info.:
- Warrendale, Penn.: Society of Automotive Engineers
- ISSN:
- 01487191
- Language:
- English
- Call no.:
- S10400
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Identification of Structural Damage Using a Sensitivity Approach Applied to Output-Only Data
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
9
Technical Paper
F-111 NATURAL LAMINAR FLOW GLOVE FLIGHT TEST DATA ANALYSIS AND BOUNDARY LAYER STABILITY ANALYSIS Contractor
National Aeronautics and Space Administration |
Society of Automotive Engineers |
10
Technical Paper
Topology and Frequency Response Function Analysis Applied to Structural Parts Aiming Mass and Cost Reduction
Society of Automotive Engineers |
Society of Automotive Engineers |
11
Technical Paper
Dynamic Modal Analysis and Optimization of a Mechanical Sensor Arm Deployment System for a C-130 Aircraft.
Society of Automotive Engineers |
6
Technical Paper
Study of the Influence of Aircraft Geometry on the Computed Flowfield During Thrust Reversers Operation
American Institute of Aeronautics and Astronautics |
12
Technical Paper
RANS's Cartographic Analysis and Geographic Information System(RAND-CAGIS): A Guide to System Use
National Aeronautics and Space Adminstration |