The blind-test activity of tiltaero project for the numerical aerodynamic investigation of a tilt rotor

ECCOMAS 2004 - European Congress on Computational Methods in Applied Sciences and Engineering

Volumn , Issue , 2004, Pages

  Visingardi, A ^a   Khier, W ^b   Decours, J ^c  

^a ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

^c ONERA   (France)

Author keywords

Blind test; Interactional aerodynamics; Rotorcraft; Tilt rotor; TILTAERO

Indexed keywords

BLIND-TEST; CFD METHODOLOGIES; EUROPEAN RESEARCH PROJECT; NUMERICAL METHODOLOGIES; ROTORCRAFT; TILT ROTOR; TILTAERO; UNSTEADY PRESSURE DISTRIBUTION;

COMPUTATIONAL METHODS; NAVIER STOKES EQUATIONS; WIND TUNNELS;

AERODYNAMIC CONFIGURATIONS;

EID: 84893503175     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Agusta S.p.A. Tilt Rotor Interactional Aerodynamics - TILTAERO - Project Nr. GRD1 2000-25610: Annex I, Description of Work. December 2000.
2. S.G. Voutsinas. The PROPWING Database. Doc. Nr. TILTAERO/WP1/NTUA/R-01/B, January 2002.
3. A. Saporiti. Trim conditions for blind tests. Doc. Nr. TILTAERO/WP1/AGUSTA/R-03/B, January 2002.
4. nd European Rotorcraft Forum, Brighton, UK, September 1996.
5. A. D'Alascio, A. Visingardi and P. Renzoni. Explicit Kutta Condition Correction for Rotary Wing Flows. 19th World Conference on the Boundary Element Method, Rome, Italy, September 1997.
6. D.R. Clark and B. Maskew. Calculation of Unsteady Rotor Blade Loads and Blade/Fuselage Interference. II International Conference on Rotorcraft Basic Research, College Park, U.S.A., February. 1988.
7. K. Becker, N. Kroll, C.C. Rossow and F. Thiele. The MEGAFLOW project Aerospace Sci. Technol. 4 (2000) 223-237.
8. A. Jameson, W. Schmidt and E. Türkei. Numerical Solutions of the Euler Equations by Finite Volume Methods using Runge-Kutta Time-Stepping Schemes. AIAA-Paper 81-1259, 1981.
9. R. Heinrich, K. Pahlke, H. Bleecke. A Three-Dimensional Dual-Time Stepping Method for the Solution of the Unsteady Navier-Stokes Equations. Proceedings of the Conference Unsteady Aerodynamics, London, Paper No. 5, 1996.
10. A. Jameson. A Time Dependent Calculation using Multigrid, with Applications to Unsteady Flows past Airfoils and Wings AIAA Paper, 91-1596, 1991.
11. L. Cambier and M. Gazaix. ElsA, An efficient object-oriented solution to CFD complexity. 40th AIAA Aerospace Science and Exhibit, Reno, NV, USA, 2002.
12. T. Renaud. Application of the actuator disk model for rotor/fuselage interaction computations with the elsA software. Technical Report ONERA RT64/06082, April 2003.
13. C. Benoít, M.-C. Le Pape and G. Jeanfaivre. Improvement of the robustness of the chimera method. Exhibit, Saint-Louis, USA, June 2002.
14. th AIAA Computational Fluid Dynamics Conference, San Diego, CA, June 1995.