Fluid structure interaction simulation on the F/A-18 vertical tail

40th AIAA Fluid Dynamics Conference

Volumn , Issue , 2010, Pages

  Guillaume, M ^a   Gehri, A ^a   Stephani, P ^a   Vos, J ^b   Mandanis, G ^c  

^a RUAG Aviation/Aerodynamics ^*  (Switzerland)

^b PSE B   (Switzerland)

^c M at M GmbH   (Switzerland)

Author keywords

[No Author keywords available]

Indexed keywords

AERO-ELASTIC SIMULATIONS; BOEING COMPANIES; CFD CODES; CFD MODELS; COMPUTATIONAL FLUID DYNAMICS CODES; DATA BASE; DESIGN SPECTRUM; DYNAMIC DESIGN; EARLY DESIGN PHASE; FATIGUE TESTS; FLIGHT LOADS; FLUCTUATING LOADS; FLUID-STRUCTURES; FULL-SCALE FATIGUE TEST; INTERNATIONAL COLLABORATIONS; LEADING EDGE EXTENSION; LOAD ANALYSIS; NAVIER STOKES; ORIGINAL EQUIPMENT MANUFACTURERS; STEADY-STATE VALUES; SWISS F/A-18; VERTICAL TAIL;

BUFFETING; DYNAMIC ANALYSIS; DYNAMIC LOADS; FATIGUE TESTING; FLUID DYNAMICS; FLUIDS; INTERNATIONAL COOPERATION; STRUCTURAL DESIGN; STRUCTURAL INTEGRITY; VORTEX FLOW;

COMPUTATIONAL FLUID DYNAMICS;

EID: 78649490195     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. M. Guillaume, B. Bucher, M. Godinat, J. Hawkins, I. Pfiffner, J. Weiss, M. Gottier, and G. Mandanis, The Swiss F/A-18 Full Scale Fatigue Test. International Committee on Aeronautical Fatigue, ICAF conference in Toulouse 2001 F, ICAF-Doc. 2289/2001
2. C. Farhat, M. Lesoinne, N. Maman. Mixed explicit/implicit time integration of coupled aero-elastic problems: three-field formulation, geometric conservation and distributed solution. International Journal of Numerical Methods in Fluid, Vol. 21, 1995, no. 10, pp.807-835.
3. J. Smith, Aeroelastic Functionality in Edge Initial Implementation and Validation, FOI Report R-1485-SE, 2005.
4. E.C. Yates Jr. AGARD Standard Aero-elastic Configurations for Dynamic Response 1: Wing 445.6 AGARD R-765, 1988, NASA TM-100492, 1987.
5. G.S. L. Goura, Time marching analysis of flutter using Computational Fluid Dynamics. Ph.D thesis, University of Glasgow, 2001.
6. Spekreijse S.P., Prananta B.B., Kok J.C. A simple, robust and fast algorithm to compute deformations of multi block structured grids, NLR-TP-2002-105, 2002.
7. Larry A. Meyn Full Scale Wind-Tunnel Studies of F/A-18 Tail Buffet Journal of Aircraft Vol. 33, No. 3, May-June 1996
8. Essam F. Sheta Alleviation of Vertical Tail Buffeting of F/A-18 Aircraft, Journal of Aircraft Vol. 41, No. 2, March-April 2004