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Volumn , Issue , 2002, Pages

Reynolds numbers considerations for supersonic flight

Author keywords

[No Author keywords available]

Indexed keywords

AERO-DYNAMIC PERFORMANCE; AIRCRAFT OPERATIONS; COMPUTATIONAL RESULTS; FLOW CHARAC-TERISTICS; HIGH REYNOLDS NUMBER; LANDING CONDITIONS; LOW REYNOLDS NUMBER; SUPERSONIC FLIGHTS;

EID: 84896693786     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (57)
  • 6
    • 0033905128 scopus 로고    scopus 로고
    • Wind-Tunnel Techniques to Successfully Predict F/A-18E In-Flight Lift and Drag
    • Jan- Feb
    • Niewald, P.W., and Parker, S.L., "Wind-Tunnel Techniques to Successfully Predict F/A-18E In-Flight Lift and Drag", Journal Of Aircraft, Vol. 37, No. 1, Jan- Feb 2000, pp 9-14
    • (2000) Journal of Aircraft , vol.37 , Issue.1 , pp. 9-14
    • Niewald, P.W.1    Parker, S.L.2
  • 7
    • 0033898211 scopus 로고    scopus 로고
    • Flight-Test Techniques Employed To Successfully Verify F/A-18E In-Flight Lift and Drag
    • Mar - Apr
    • Niewald, P.W., and S.L. Parker,"Flight-Test Techniques Employed To Successfully Verify F/A-18E In-Flight Lift and Drag", Journal of Aircraft Vol. 37, No 2, Mar - Apr 2000, pp 194-200
    • (2000) Journal of Aircraft , vol.37 , Issue.2 , pp. 194-200
    • Niewald, P.W.1    Parker, S.L.2
  • 9
    • 0018530068 scopus 로고
    • Real Flow Limitations in Supersonic Airplane Design
    • Oct
    • Kulfan, R.M., Sigalla, A., "Real Flow Limitations in Supersonic Airplane Design:, Journal of Aircraft, Vol. 16 No. 10, pp 645-658, Oct. 1979
    • (1979) Journal of Aircraft , vol.16 , Issue.10 , pp. 645-658
    • Kulfan, R.M.1    Sigalla, A.2
  • 14
    • 0012274446 scopus 로고
    • Possible Types of Flow at Swept Leading Edges
    • Feb
    • Stanbrook, A., and Squire, L.C., "Possible Types of Flow at Swept Leading Edges", The Aeronautical Quarterly, Feb 1964, pp 72-82
    • (1964) The Aeronautical Quarterly , pp. 72-82
    • Stanbrook, A.1    Squire, L.C.2
  • 16
    • 0015039667 scopus 로고
    • Predictions of Vortex-Lift Characteristics by a Leading-Edge-Suction-Analogy
    • April
    • Polhamus, E.C., "Predictions of Vortex-Lift Characteristics by a Leading-Edge-Suction-Analogy", Journal of Aircraft, Vol.8, No. 4, April 1971
    • (1971) Journal of Aircraft , vol.8 , Issue.4
    • Polhamus, E.C.1
  • 17
    • 0022880574 scopus 로고
    • An Overview of the Fundamental Aerodynamics Branch's Research Activities in Wing Leading-Edge Vortex Flows at Supersonic Speeds
    • NASA Conference Publication 2416 Oct
    • Miller, D. S., Wood, R. M., and Covell, P. F., "An Overview of the Fundamental Aerodynamics Branch's Research Activities in Wing Leading-Edge Vortex Flows at Supersonic Speeds", NASA Conference Publication 2416, Vortex Flow Aerodynamics, Vol 1 pp 349-378, Oct 1985
    • (1985) Vortex Flow Aerodynamics , vol.1 , pp. 349-378
    • Miller, D.S.1    Wood, R.M.2    Covell, P.F.3
  • 20
    • 0035516863 scopus 로고    scopus 로고
    • Single-Point and Multipoint Aerodynamic Shape Optimization of High-Speed Civil Aircraft
    • Nov.-Dec
    • Cliff, S.E., Reuther, J.J., Saunders, D.A., and Hicks, R.M., "Single-Point and Multipoint Aerodynamic Shape Optimization of High-Speed Civil Aircraft", Lournal of Aircraft, Vol. 38, No.6, Nov.-Dec., 2001, pp 997-1005
    • (2001) Lournal of Aircraft , vol.38 , Issue.6 , pp. 997-1005
    • Cliff, S.E.1    Reuther, J.J.2    Saunders, D.A.3    Hicks, R.M.4
  • 21
    • 0035389988 scopus 로고    scopus 로고
    • Flap- Deflection Optimization for Transonic Cruise Performance Improvement of Supersonic Transport Wing
    • Jul.-Aug
    • Kim, H-J., Shigeru, O., and Nakahashi, K., "Flap- Deflection Optimization for Transonic Cruise Performance Improvement of Supersonic Transport Wing", Journal of Aircraft, Vol. 38, No. 4, Jul.-Aug,. 2001, pp 709-717
    • (2001) Journal of Aircraft , vol.38 , Issue.4 , pp. 709-717
    • Kim, H.-J.1    Shigeru, O.2    Nakahashi, K.3
  • 23
    • 38149057944 scopus 로고    scopus 로고
    • Historic Background on Flat Plate Turbulent Flow Skin Friction and Boundary Layer Growth
    • Dec 01, 1999, NASA/CP-1999- 209692/Vol. 1/Pt. 1
    • Kulfan, R. M., "Historic Background on Flat Plate Turbulent Flow Skin Friction and Boundary Layer Growth.", 1998 NASA High-Speed Research Program Aerodynamic Performance Workshop, Vol. 1, Part 1 Page: 477-513, Dec 01, 1999, NASA/CP-1999- 209692/Vol. 1/Pt. 1
    • 1998 NASA High-Speed Research Program Aerodynamic Performance Workshop , vol.1 , Issue.PART 1 , pp. 477-513
    • Kulfan, R.M.1
  • 30
    • 0028486598 scopus 로고
    • Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications
    • August
    • Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications:, AIAA Journal, vol. 32, no. 8, August 1994, pp. 357-372
    • (1994) AIAA Journal , vol.32 , Issue.8 , pp. 357-372
    • Menter, F.R.1
  • 34
    • 77958537212 scopus 로고
    • The Problem of Roughness Drag at Supersonic Speeds
    • NASA SP-124, May
    • Czarnecki, K.R., "The Problem of Roughness Drag at Supersonic Speeds", NASA SP-124, Conference on Aircraft Aerodynamics, May 1966
    • (1966) Conference On Aircraft Aerodynamics
    • Czarnecki, K.R.1
  • 37
    • 0029761838 scopus 로고
    • Review of the Physics of Swept-Shock/Boundary Layer Interactions
    • Panaras, A.G., "Review of the Physics of Swept-Shock/Boundary Layer Interactions", Prog. Aerospace Sci. vol 31, pp 173-244, 1995
    • (1995) Prog. Aerospace Sci , vol.31 , pp. 173-244
    • Panaras, A.G.1
  • 39
    • 0022909475 scopus 로고
    • Vortex Lift Research: Early Contributions and Some Current Challenges
    • NASA Conference Publication 2416, Oct
    • Polhamus, E.C., Vortex Lift Research: Early Contributions and Some Current Challenges", NASA Conference Publication 2416, Vortex Flow Aerodynamics, Vol 1 pp 1-30, Oct 1985
    • (1985) Vortex Flow Aerodynamics , vol.1 , pp. 1-30
    • Polhamus, E.C.1
  • 40
    • 84896824525 scopus 로고
    • Some Non-planar Concepts and Current Challenges
    • Leading-Edge Vortex Research:, NASA Conference Publication 2416, Oct
    • Leading-Edge Vortex Research: "Some Non-planar Concepts and Current Challenges", NASA Conference Publication 2416, Vortex Flow Aerodynamics, Vol 1 pp 31-64, Oct 1985
    • (1985) Vortex Flow Aerodynamics , vol.1 , pp. 31-64
  • 42
    • 0022874269 scopus 로고
    • In-Flight and Wind Tunnel Leading Edge Vortex Study on the F-106B Airplane
    • NASA Conference Publication 2416, Oct
    • Lamar, J.E., "In-Flight and Wind Tunnel Leading Edge Vortex Study on the F-106B Airplane", NASA Conference Publication 2416, Vortex Flow Aerodynamics, Vol 1 pp 187-202, Oct 1985
    • (1985) Vortex Flow Aerodynamics , vol.1 , pp. 187-202
    • Lamar, J.E.1
  • 44
    • 84896822402 scopus 로고
    • Comparison of Theoretical and Experimental Pressure distributions on an Arrow Wing Configuration at Transonic Speeds
    • NASA SP- 347
    • Manro, M.E., Tinoco, E.N., Bobbit, P.H., and Rogers, J. T., "Comparison of Theoretical and Experimental Pressure distributions on an Arrow Wing Configuration at Transonic Speeds", AERODYNAMIC ANALYSIS REQUIRING ADVANCED COMPUTERS, NASA SP- 347, PP 1141-1188, 1975
    • (1975) AERODYNAMIC ANALYSIS REQUIRING ADVANCED COMPUTERS , pp. 1141-1188
    • Manro, M.E.1    Tinoco, E.N.2    Bobbit, P.H.3    Rogers, J.T.4
  • 46
    • 0023994307 scopus 로고
    • Comparison of Euler and Navier Stokes Solutions for Vortex Flow Over a Delta Wing
    • April
    • Rizzi, A., Muller, B., "Comparison of Euler and Navier Stokes Solutions for Vortex Flow Over a Delta Wing", Aeronautical Journal, pp 145-153, April 1988
    • (1988) Aeronautical Journal , pp. 145-153
    • Rizzi, A.1    Muller, B.2
  • 48
    • 84896893472 scopus 로고
    • Transonic Navier-Stokes Calculations About a 65O Delta Wing
    • Nov
    • Londenberg, W.K., "Transonic Navier-Stokes Calculations About a 65O Delta Wing", NASA Contractor Report 4635, Nov. 1994
    • (1994) NASA Contractor Report , pp. 4635
    • Londenberg, W.K.1
  • 49
    • 0026838276 scopus 로고
    • Computational Study of Incipient Leading Edge Separation on a Supersonic Delta Wing
    • Mar - April
    • McMillin, S.N., Pittman, J.L., and Thomas, J. L., "Computational Study of Incipient Leading Edge Separation on a Supersonic Delta Wing", Journal of Aircraft Vol 29, No. 2, Mar - April 1992
    • (1992) Journal of Aircraft , vol.29 , Issue.2
    • McMillin, S.N.1    Pittman, J.L.2    Thomas, J.L.3
  • 50
    • 0026224099 scopus 로고
    • Thin-Layer Full Navier-Stokes Simulations over a supersonic Delta Wing
    • September
    • Webster, W.P., and Shang, J.S., "Thin-Layer Full Navier-Stokes Simulations over a supersonic Delta Wing", AIAA Journal Vol. 29, No. 9, September 1991, pp 1363-1369
    • (1991) AIAA Journal , vol.29 , Issue.9 , pp. 1363-1369
    • Webster, W.P.1    Shang, J.S.2
  • 51
    • 85003238638 scopus 로고
    • Flow Patterns and Aerodynamic Characteristics of a Wing - Strake Configuration
    • May
    • Liu, M.J., et al.:Flow Patterns and Aerodynamic Characteristics of a Wing - Strake Configuration", Journal of Aircraft, Vol. 17, No. 5, pp 332-337, May 1980
    • (1980) Journal of Aircraft , vol.17 , Issue.5 , pp. 332-337
    • Liu, M.J.1
  • 52
    • 0025446832 scopus 로고
    • Navier-Stokes Computations of Flow around a Round-Edged Double-Delta Wing
    • June
    • Hsu, C.H., and Liu, C. H., "Navier-Stokes Computations of Flow around a Round-Edged Double-Delta Wing", AIAA Journal Vol. 28, NO. 6, June 1990, pp 961-968
    • (1990) AIAA Journal , vol.28 , Issue.6 , pp. 961-968
    • Hsu, C.H.1    Liu, C.H.2
  • 54
    • 0022862291 scopus 로고
    • Extensions of the Concept of Suction Analogy to Prediction of Vortex Lift Effect
    • NASA CP 2416 Oct
    • Lan, C.E., "Extensions of the Concept of Suction Analogy to Prediction of Vortex Lift Effect.", NASA CP 2416, VORTEX FLOW AERODYNAMICS, Oct 1985, pp 65-84
    • (1985) VORTEX FLOW AERODYNAMICS , pp. 65-84
    • Lan, C.E.1
  • 55
    • 85002934362 scopus 로고
    • Navier- Stokes Solutions About the F/A-18 Forebody-Leading- Edge Extension Configuration
    • Sept
    • Gharrari, F., Luckring, J.M., and Thomas, J.L., "Navier- Stokes Solutions About the F/A-18 Forebody-Leading- Edge Extension Configuration", Journal of Aircraft, Vol. 27, NO. 9, Sept 1990, pp 737-748
    • (1990) Journal of Aircraft , vol.27 , Issue.9 , pp. 737-748
    • Gharrari, F.1    Luckring, J.M.2    Thomas, J.L.3
  • 57
    • 0025843737 scopus 로고    scopus 로고
    • Computation of Navier- Stokes Solutions Exhibiting Asymmetric Vortices
    • Siclari, M.J., and Marconi, F., "Computation of Navier- Stokes Solutions Exhibiting Asymmetric Vortices", Aiaa Journal Vol. 29, NO. 1, pp32-42
    • AIAA Journal , vol.29 , Issue.1 , pp. 32-42
    • Siclari, M.J.1    Marconi, F.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.