Aeroelastic analysis of an SST typed wing with a trailing edge flap using a Chimera grid approach

AIAA Paper

Volumn , Issue , 2004, Pages 10226-10233

  Utaka, Yasukazu ^a   Nakamichi, Jiro ^b,c  

^a MITSUBISHI HEAVY INDUSTRIES LTD   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c Struct/Materials Research Center   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

CURVILINEAR COORDINATES; MACH NUMBERS; PRESSURE COEFFICIENTS;

AERODYNAMICS; AEROSPACE ENGINEERING; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; ELASTICITY; INTEGRATION; NAVIER STOKES EQUATIONS; PRESSURE DISTRIBUTION; TRANSONIC FLOW; WIND TUNNELS;

WINGS;

EID: 2942744681     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Nixon, D., Unsteady Transonic Aerodynamics, American Institute of Aeronautics and Astronautics, Washington, D.C., 1988.
2. Kheirandish H., Beppu G., Nakamichi J., "Computational Investigation of Wing Flutter," International Journal of Computational Fluid Dynamics, vol. 12, 1999, pp.279-290.
3. Yee H. and Klopfer G. H. and Montagne J. L., "High Resolution Shock-Capturing Schemes for Inviscid and Viscous Hypersonic Flows," NASA TM-100097, 1988.
4. Bate K.J. and Wilson E.L., "Numerical Methods in Finite Element Analysis," Prentic-Hall, 1976.
5. Kamiya, H., Kaiden, T. and Masuda, K., "Numerical Simulation of SST with Nacelle Installation and Flap Deployment," AIAA Paper 2001-1007, 2001.
6. Nakamichi J., "Calculation of Unsteady Navier-Stokes Equations Around an Oscillating 3-D Wing Using Moving Grid System," AIAA Paper 87-1158-CP, 1987.