메뉴 건너뛰기




Volumn 41, Issue 4, 2004, Pages 798-810

Computational-fluid-dynamics-based enhanced indicial aerodynamic models

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; CORRELATION METHODS; DATABASE SYSTEMS; LINEARIZATION; MATHEMATICAL MODELS; PROBLEM SOLVING; UNSTEADY FLOW; VORTEX FLOW;

EID: 4344614202     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.12419     Document Type: Article
Times cited : (20)

References (21)
  • 1
    • 0030247548 scopus 로고    scopus 로고
    • Subsonic unsteady aerodynamics caused by gusts using the indicial method
    • Leishman, J. G., "Subsonic Unsteady Aerodynamics Caused by Gusts Using the Indicial Method," Journal of Aircraft, Vol. 33, No. 5, 1996, pp. 869-879.
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 869-879
    • Leishman, J.G.1
  • 3
    • 0038839479 scopus 로고
    • Two and three dimensional unsteady lift problems in high speed flight
    • Jan.
    • Lomax, H., Heaslet, M. A., Fuller, F. B., and Sluder, L., "Two and Three Dimensional Unsteady Lift Problems in High Speed Flight," NACA Rept. 1077, Jan. 1952.
    • (1952) NACA Rept. , vol.1077
    • Lomax, H.1    Heaslet, M.A.2    Fuller, F.B.3    Sluder, L.4
  • 5
    • 4344572054 scopus 로고
    • Determination of indicial lift and moment of a two-dimensional pitching airfoil at subsonic mach numbers from oscillatory coefficients with numerical calculations for a mach number of 0.7
    • Feb.
    • Mazelsky, B., "Determination of Indicial Lift and Moment of a Two-Dimensional Pitching Airfoil at Subsonic Mach Numbers from Oscillatory Coefficients with Numerical Calculations for a Mach number of 0.7," NACA TN 2613, Feb. 1952.
    • (1952) NACA TN , vol.2613
    • Mazelsky, B.1
  • 6
    • 0008358667 scopus 로고
    • The aerodynamic force on an airfoil in a moving gust
    • Miles, J. W., "The Aerodynamic Force on an Airfoil in a Moving Gust," Journal of Aeronautical Sciences, Vol. 23, No. 11, 1956, pp. 1044-1050.
    • (1956) Journal of Aeronautical Sciences , vol.23 , Issue.11 , pp. 1044-1050
    • Miles, J.W.1
  • 7
    • 6044250654 scopus 로고
    • Lift and moment responses to penetration of sharp-edged traveling vertical gusts, with application to penetration of weak blast waves
    • May
    • Drischler, J. A., and Diederich, F. W., "Lift and Moment Responses to Penetration of Sharp-Edged Traveling Vertical Gusts, with Application to Penetration of Weak Blast Waves," NACA TN 3956, May 1957.
    • (1957) NACA TN , vol.3956
    • Drischler, J.A.1    Diederich, F.W.2
  • 8
    • 0009460424 scopus 로고
    • Numerical determination of indicial lift and moment functions for a two-dimensional sinking and pitching airfoil at mach numbers 0.5 and 0.6
    • July
    • Mazelsky, B., and Drischler, J. A., "Numerical Determination of Indicial Lift and Moment Functions for a Two-Dimensional Sinking and Pitching Airfoil at Mach Numbers 0.5 and 0.6," NASA TN 2739, July 1952.
    • (1952) NASA TN , vol.2739
    • Mazelsky, B.1    Drischler, J.A.2
  • 9
    • 0031273412 scopus 로고    scopus 로고
    • Unsteady aerodynamics of airfoils encountering traveling gusts and vortices
    • Leishman, J. G., "Unsteady Aerodynamics of Airfoils Encountering Traveling Gusts and Vortices," Journal of Aircraft, Vol. 34, No. 6, 1997, pp. 719-729.
    • (1997) Journal of Aircraft , vol.34 , Issue.6 , pp. 719-729
    • Leishman, J.G.1
  • 11
    • 0012376207 scopus 로고
    • Use of source distribution for evaluating theoretical aerodynamics of thin finite wings at supersonic speeds
    • June
    • Evvard, J. C., "Use of Source Distribution for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds," NACA Rept. 951, June 1950.
    • (1950) NACA Rept. , vol.951
    • Evvard, J.C.1
  • 12
    • 0031189057 scopus 로고    scopus 로고
    • The direct calculation of indicial lift response of a wing using computational fluid dynamics
    • Singh, R., and Baeder, J. D., "The Direct Calculation of Indicial Lift Response of a Wing Using Computational Fluid Dynamics," Journal of Aircraft, Vol. 35, No. 4, 1997, pp. 465-471.
    • (1997) Journal of Aircraft , vol.35 , Issue.4 , pp. 465-471
    • Singh, R.1    Baeder, J.D.2
  • 13
    • 34147213648 scopus 로고    scopus 로고
    • Generalized moving gust response using CFD with application to airfoil-vortex interaction
    • Atlanta, GA, June
    • Singh, R., and Baeder, J. D., "Generalized Moving Gust Response Using CFD with Application to Airfoil-Vortex Interaction," Proceedings of the 15th AIAA Applied Aerodynamics Conference, Atlanta, GA, June 1999; also AIAA Paper 97-2208.
    • (1999) Proceedings of the 15th AIAA Applied Aerodynamics Conference
    • Singh, R.1    Baeder, J.D.2
  • 14
    • 85039496593 scopus 로고    scopus 로고
    • Singh, R., and Baeder, J. D., "Generalized Moving Gust Response Using CFD with Application to Airfoil-Vortex Interaction," Proceedings of the 15th AIAA Applied Aerodynamics Conference, Atlanta, GA, June 1999; also AIAA Paper 97-2208.
    • AIAA Paper , vol.97 , Issue.2208
  • 15
    • 0027591735 scopus 로고
    • TURNS: A free wake Euler/Navier-Stokes numerical method for helicopter rotors
    • Srinivasan, G. R., and Baeder, J. D., "TURNS: A Free Wake Euler/Navier-Stokes Numerical Method for Helicopter Rotors," AIAA Jour-nal, Vol. 31, No. 5, 1993, pp. 959-962.
    • (1993) AIAA Journal , vol.31 , Issue.5 , pp. 959-962
    • Srinivasan, G.R.1    Baeder, J.D.2
  • 18
    • 0011107057 scopus 로고
    • Computation of helicopter rotor wake geometry and its influence on rotor harmonic airloads
    • Dept. of Aerospace Engineering, Massachusetts Inst. of Technology, Cambridge, MA, March
    • Scully, M. P., "Computation of Helicopter Rotor Wake Geometry and Its Influence on Rotor Harmonic Airloads," ASRL TR 178-1, Dept. of Aerospace Engineering, Massachusetts Inst. of Technology, Cambridge, MA, March 1975.
    • (1975) ASRL TR , vol.178 , Issue.1
    • Scully, M.P.1
  • 19
    • 0021600203 scopus 로고
    • Practical computation of unsteady lift
    • Beddoes, T. S., "Practical Computation of Unsteady Lift," Vertica, Vol. 8, No. 1, 1984, pp. 55-71.
    • (1984) Vertica , vol.8 , Issue.1 , pp. 55-71
    • Beddoes, T.S.1
  • 20
    • 0004081663 scopus 로고
    • Vanderplaats, Miura and Associates, Inc., April
    • "DOT Users Manual," ver. 4.00, Vanderplaats, Miura and Associates, Inc., April 1993.
    • (1993) "DOT Users Manual," Ver. 4.00
  • 21
    • 0024088694 scopus 로고
    • Validation of approximate indicial aerodynamics functions for two-dimensional subsonic flow
    • Leishman, J. G., "Validation of Approximate Indicial Aerodynamics Functions for Two-Dimensional Subsonic Flow," AIAA Journal, Vol. 25, No. 10, 1988, pp. 914-922.
    • (1988) AIAA Journal , vol.25 , Issue.10 , pp. 914-922
    • Leishman, J.G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.