메뉴 건너뛰기




Volumn 42, Issue 9, 2004, Pages 1775-1787

Overset field-panel method for unsteady transonic aerodynamic influence coefficient matrix generation

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; GREEN'S FUNCTION; NAVIER STOKES EQUATIONS; OPTIMIZATION; PERTURBATION TECHNIQUES; PROBLEM SOLVING; TRANSONIC AERODYNAMICS; WINGS;

EID: 4944250275     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.4390     Document Type: Article
Times cited : (39)

References (19)
  • 1
    • 3343014691 scopus 로고
    • New method for non-planar configurations
    • Rodden, W. P., Giesing, J. P., and Kalam, T. P., "New Method for Non-planar Configurations," AGARD, CP-80-71, Pt. 2, No. 4, 1971.
    • (1971) AGARD , vol.CP-80-71 , Issue.4 PART 2
    • Rodden, W.P.1    Giesing, J.P.2    Kalam, T.P.3
  • 2
    • 0027664805 scopus 로고
    • Unsteady subsonic aerodynamics for bodies and wings with external stores including wake effort
    • Chen, P. C., Lee, H. W., and Liu, D. D., "Unsteady Subsonic Aerodynamics for Bodies and Wings with External Stores Including Wake Effort," Journal of Aircraft, Vol. 30, No. 5, 1993, pp. 618-628.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 618-628
    • Chen, P.C.1    Lee, H.W.2    Liu, D.D.3
  • 3
    • 0025388451 scopus 로고
    • Unsteady supersonic computation of arbitrary wing-body configurations including external stores
    • Chen, P. C., and Liu, D. D., "Unsteady Supersonic Computation of Arbitrary Wing-Body Configurations Including External Stores," Journal of Aircraft, Vol. 27, No. 2, 1990, pp. 108-116.
    • (1990) Journal of Aircraft , vol.27 , Issue.2 , pp. 108-116
    • Chen, P.C.1    Liu, D.D.2
  • 4
    • 0022309751 scopus 로고
    • Calculation of 3D unsteady transonic potential flows by a field panel method
    • Aachen, Germany
    • Voss, R., "Calculation of 3D Unsteady Transonic Potential Flows by a Field Panel Method," 2nd International Symposium on Aeroelasticity and Structural Dynamics, Aachen, Germany, 1985, pp. 33-46.
    • (1985) 2nd International Symposium on Aeroelasticity and Structural Dynamics , pp. 33-46
    • Voss, R.1
  • 6
    • 0039377023 scopus 로고
    • Nonlinear green's function method for unsteady transonic flows
    • edited by D. Nixon, Progress in Astronautics and Aeronautics, AIAA, New York
    • Tseng, K., and Merino, L., "Nonlinear Green's Function Method for Unsteady Transonic Flows," Transonic Aerodynamics, edited by D. Nixon, Vol. 81, Progress in Astronautics and Aeronautics, AIAA, New York, 1982, pp. 565-603.
    • (1982) Transonic Aerodynamics , vol.81 , pp. 565-603
    • Tseng, K.1    Merino, L.2
  • 7
    • 0016057538 scopus 로고
    • Analysis of embedded shock waves calculated by relaxation methods
    • Murman, E. M., "Analysis of Embedded Shock Waves Calculated by Relaxation Methods," AIAA Journal, Vol. 12, No. 5, 1974, pp. 626-633.
    • (1974) AIAA Journal , vol.12 , Issue.5 , pp. 626-633
    • Murman, E.M.1
  • 9
    • 0023866130 scopus 로고    scopus 로고
    • An efficient method for computing unsteady transonic aerodynamics of swept wings with control surfaces
    • Liu, D. D., Kao, Y. F., and Fung, K. Y., "An Efficient Method for Computing Unsteady Transonic Aerodynamics of Swept Wings with Control Surfaces," Journal of Aircraft, Vol. 25, No. 1, 1998, pp. 25-31.
    • (1998) Journal of Aircraft , vol.25 , Issue.1 , pp. 25-31
    • Liu, D.D.1    Kao, Y.F.2    Fung, K.Y.3
  • 11
    • 4944231952 scopus 로고
    • Transonic wind-tunnel tests on an oscillating wing with external stores
    • Sept.
    • Tijdeman, H., and Nunen, J. W. G. v., "Transonic Wind-Tunnel Tests on an Oscillating Wing with External Stores," AFFDL-TR-78-189, Pt. 2, Sept. 1978.
    • (1978) AFFDL-TR-78-189 , Issue.PART. 2
    • Tijdeman, H.1    Nunen, J.W.G.V.2
  • 12
    • 4944249991 scopus 로고
    • Experimental determination on a rectangular wing oscillating in the first bending mode for mach numbers from 0.24 to 1.30
    • Dec.
    • Lessing, H. C., Troutman, J. L., and Menees, G. P., "Experimental Determination on a Rectangular Wing Oscillating in the First Bending Mode for Mach Numbers from 0.24 to 1.30," NASA TND-33, Dec. 1960.
    • (1960) NASA TND-33
    • Lessing, H.C.1    Troutman, J.L.2    Menees, G.P.3
  • 13
    • 4944234003 scopus 로고
    • LANN wing test program: Acquisition and application of unsteady transonic data for evaluation of three-dimensional computational methods
    • Feb.
    • Malone, J. B., and Ruo, S. Y., "LANN Wing Test Program: Acquisition and Application of Unsteady Transonic Data for Evaluation of Three-Dimensional Computational Methods," AFWAL-TR-83-6006, Feb. 1983.
    • (1983) AFWAL-TR-83-6006
    • Malone, J.B.1    Ruo, S.Y.2
  • 14
    • 0004826888 scopus 로고
    • AGARD standard aeroelastic configurations for dynamic response I-wing 445.6
    • Aug.
    • Yates, E. C., "AGARD Standard Aeroelastic Configurations for Dynamic Response I-Wing 445.6," NASA TM 100492, Aug. 1987.
    • (1987) NASA TM 100492
    • Yates, E.C.1
  • 15
    • 4944240733 scopus 로고
    • Experimental flutter results of a cambered supercritical wing on a pitch and plunge apparatus
    • NASA Langley Research Center, Hampton, VA, May
    • Farmer, M. G., and Rivera, J. A., "Experimental Flutter Results of a Cambered Supercritical Wing on a Pitch and Plunge Apparatus," Aerospace Flutter and Dynamics Council Meeting, NASA Langley Research Center, Hampton, VA, May 1988.
    • (1988) Aerospace Flutter and Dynamics Council Meeting
    • Farmer, M.G.1    Rivera, J.A.2
  • 16
    • 0034276174 scopus 로고    scopus 로고
    • Damping perturbation method for flutter solution: The g-method
    • Chen, P. C., "Damping Perturbation Method for Flutter Solution: The g-Method," AIAA Journal, Vol. 38, No. 9, 2000, pp. 1519-1524.
    • (2000) AIAA Journal , vol.38 , Issue.9 , pp. 1519-1524
    • Chen, P.C.1
  • 17
    • 0021698185 scopus 로고
    • A practical method for predicting transonic wing flutter phenomena
    • Paper 84-1.7.1, Toulouse, France, Sept.
    • Yonemoto, Koichi, "A Practical Method for Predicting Transonic Wing Flutter Phenomena," International Council of the Aeronautical Sciences, Paper 84-1.7.1, Toulouse, France, Sept. 1984.
    • (1984) International Council of the Aeronautical Sciences
    • Yonemoto, K.1
  • 18
    • 20544473635 scopus 로고
    • Numerical simulation of transonic flutter of a high-aspect-ratio transport wing
    • Japan, Aug.
    • Isogai, K., "Numerical Simulation of Transonic Flutter of a High-Aspect-Ratio Transport Wing," National Aerospace Lab., Rept. TR-776T, Japan, Aug. 1983.
    • (1983) National Aerospace Lab., Rept. TR-776T
    • Isogai, K.1
  • 19
    • 4944249992 scopus 로고
    • Technique for accurate, efficient computational of unsteady transonic flow
    • Jan.
    • Shieh, T. H., Schoen, J. G., and Fung, K. Y., "Technique for Accurate, Efficient Computational of Unsteady Transonic Flow," AIAA Paper 91-0597, Jan. 1991.
    • (1991) AIAA Paper , vol.91 , Issue.597
    • Shieh, T.H.1    Schoen, J.G.2    Fung, K.Y.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.