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Volumn , Issue , 2010, Pages

Comparison of CFD predictions with shuttle global flight thermal imagery and discrete surface measurements

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY-LAYER TRANSITION; CFD CODES; CFD MODELS; CFD SIMULATIONS; FLIGHT DATA; HYPERSONIC FLIGHTS; INFRARED IMAGES; INFRARED MEASUREMENTS; MODEL RESULTS; SHEAR-STRESS TRANSPORT; SPACE SHUTTLE ORBITER; SURFACE TEMPERATURE MEASUREMENT; SURFACE TEMPERATURE PREDICTION; SURFACE TEMPERATURES; TEMPERATURE TRENDS; THERMAL IMAGERY; THERMOCOUPLE MEASUREMENTS; TWO-EQUATION TURBULENCE MODELS;

EID: 78649855839     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (18)

References (28)
  • 8
    • 0000737072 scopus 로고    scopus 로고
    • Data-parallel line relaxation method for the Navier-stokes equations
    • Sept.
    • Wright, M. J., Candler, G. V., and Bose, D., "Data-Parallel Line Relaxation Method for the Navier-Stokes Equations," AIAA Journal, Vol. 36, No. 9, Sept. 1998, pp. 1603-1609.
    • (1998) AIAA Journal , vol.36 , Issue.9 , pp. 1603-1609
    • Wright, M.J.1    Candler, G.V.2    Bose, D.3
  • 13
    • 0028486598 scopus 로고
    • Two-equation eddy-viscosity turbulence models for engineering applications
    • Aug.
    • Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol. 32, No. 8, Aug. 1994, pp. 1598-1605.
    • (1994) AIAA Journal , vol.32 , Issue.8 , pp. 1598-1605
    • Menter, F.R.1
  • 14
    • 85014968673 scopus 로고
    • A finite-difference method for calculating compressible laminar and turbulent boundary layers
    • Sept.
    • Cebeci, T. and Smith, A. M. O., "A Finite-Difference Method for Calculating Compressible Laminar and Turbulent Boundary Layers," Journal of Basic Engineering, Sept. 1970, pp. 523-535.
    • (1970) Journal of Basic Engineering , pp. 523-535
    • Cebeci, T.1    Smith, A.M.O.2
  • 18
    • 0028338141 scopus 로고
    • Characteristics of the shuttle orbiter leeside flow during a re-entry condition
    • Jan.
    • Kleb, W. L. and Weilmuenster, K. J., "Characteristics of the Shuttle Orbiter Leeside Flow During a Re-Entry Condition," Journal of Spacecraft and Rockets, Vol. 31, No. 1, Jan. 1994, pp. 8-16.
    • (1994) Journal of Spacecraft and Rockets , vol.31 , Issue.1 , pp. 8-16
    • Kleb, W.L.1    Weilmuenster, K.J.2
  • 19
    • 0027626039 scopus 로고
    • Solution strategy for three-dimensional configurations at hypersonic speeds
    • July-August
    • Weilmuenster, K. J. and Gnoffo, P. A., "Solution Strategy for Three-Dimensional Configurations at Hypersonic Speeds," Journal of Spacecraft and Rockets, Vol. 30, No. 4, July-August 1993, pp. 385-394.
    • (1993) Journal of Spacecraft and Rockets , vol.30 , Issue.4 , pp. 385-394
    • Weilmuenster, K.J.1    Gnoffo, P.A.2
  • 22
    • 84947734202 scopus 로고    scopus 로고
    • Loci: A deductive framework for graph-based algorithms
    • edited by S. Matsuoka, R. Oldehoeft, and M. Tholburn, Springer-Verlag, Dec.
    • Luke, E. A., "Loci: A Deductive Framework for Graph-Based Algorithms," Third International Symposium on Computing in Object-Oriented Parallel Environments (ISCOPE), edited by S. Matsuoka, R. Oldehoeft, and M. Tholburn, Springer-Verlag, Dec. 1999, pp. 142-153.
    • (1999) Third International Symposium on Computing in Object-Oriented Parallel Environments (ISCOPE) , pp. 142-153
    • Luke, E.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.