Experimental investigation of new GVT concepts for large aircraft

Proceedings of the International Modal Analysis Conference - IMAC

Volumn 2, Issue , 2001, Pages 1702-1708

  Gloth, G ^a   Degener, M ^a   Fullekrug U ^a   Fargette, P ^a   Levadoux, B ^a   Lubrina, P ^a   Gschwilm, J ^a   Sinapius, M ^a  

^a NONE

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; EIGENVALUES AND EIGENFUNCTIONS; FINITE ELEMENT METHOD; FLIGHT DYNAMICS; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; TRANSPORT AIRCRAFT;

FLUTTER STABILITY; GROUND VIBRATION TEST;

VIBRATION MEASUREMENT;

EID: 0035045599     PISSN: 10466770     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Conference Paper

References (11)

1. Modal identification of large aircraft
2. Konzepte zur Verkürzung der Standschwingungsversuchszeiten an Flugzeugen
3. Neuere Entwicklungen der experimentellen Modalanalyse in der Luft- und Raumfahrt
4. A semi-automatic modal survey test technique for complex aircraft and spacecraft structures
5. Ground vibration tests for validation of large aircraft structural dynamics
6. Using mode shape expansion techniques for pretest analysis and correlation
7. Use of finite element models for prediction of ground vibration test
8. A new method for computing optimized exciter forces in phase resonance testing
9. Computer controlled normal mode tuning
10. Computation of total response mode shapes using tuned frequency response functions
11. Frequency domain direct parameter identification for modal analysis: State space formulation