메뉴 건너뛰기




Volumn 42, Issue 1, 2005, Pages 138-147

Time-dependent coefficient reduced-order model for unsteady aerodynamics of proprotors

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT MODELS; APPROXIMATION THEORY; BOUNDARY ELEMENT METHOD; COMPUTATIONAL FLUID DYNAMICS; MATRIX ALGEBRA; PERTURBATION TECHNIQUES; TRANSFER FUNCTIONS; WINGS;

EID: 13844255215     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.4817     Document Type: Article
Times cited : (19)

References (20)
  • 1
    • 0005868145 scopus 로고
    • Dynamics of tilting proprotor aircraft in cruise flight
    • May
    • Johnson, W., "Dynamics of Tilting Proprotor Aircraft in Cruise Flight," NASA TN D-7677, May 1974.
    • (1974) NASA TN , vol.D-7677
    • Johnson, W.1
  • 4
    • 0032182448 scopus 로고    scopus 로고
    • Validation of a comprehensive aeroelastic analysis for tiltrotor aircraft
    • Srinivas, V., and Chopra, I., "Validation of a Comprehensive Aeroelastic Analysis for Tiltrotor Aircraft," Journal of the American Helicopter Society, Vol. 43, No. 4, 1998, pp. 333-341.
    • (1998) Journal of the American Helicopter Society , vol.43 , Issue.4 , pp. 333-341
    • Srinivas, V.1    Chopra, I.2
  • 5
    • 0034295236 scopus 로고    scopus 로고
    • Aeroelastic tailoring for stability augmentation and performance enhancements of tiltrotor aircraft
    • Nixon, M. W., Piatak, D. J., Corso, L. M., and Popelka, D. A., "Aeroelastic Tailoring for Stability Augmentation and Performance Enhancements of Tiltrotor Aircraft," Journal of the American Helicopter Society, Vol. 45, No. 4, 2000, pp. 270-279.
    • (2000) Journal of the American Helicopter Society , vol.45 , Issue.4 , pp. 270-279
    • Nixon, M.W.1    Piatak, D.J.2    Corso, L.M.3    Popelka, D.A.4
  • 6
    • 0038025486 scopus 로고    scopus 로고
    • Whirl flutter stability of two-bladed proprotor/pylon system in high speed flight
    • Singh, B., and Chopra, I.,"Whirl Flutter Stability of Two-Bladed Proprotor/Pylon System in High Speed Flight," Journal of the American Helicopter Society, Vol. 48, No. 2, 2003, pp. 99-107.
    • (2003) Journal of the American Helicopter Society , vol.48 , Issue.2 , pp. 99-107
    • Singh, B.1    Chopra, I.2
  • 7
    • 10244271953 scopus 로고    scopus 로고
    • Analysis of prop-rotor whirl flutter: Review and update
    • April
    • Kunz, D. L., "Analysis of Prop-Rotor Whirl Flutter: Review and Update," AIAA Paper 2002-1602, April 2002.
    • (2002) AIAA Paper , vol.2002 , Issue.1602
    • Kunz, D.L.1
  • 8
    • 0028427650 scopus 로고
    • Whirl-flutter suppression in advanced turboprop and propfans by active control techniques
    • Nitzsche, F.,"Whirl-Flutter Suppression in Advanced Turboprop and Propfans by Active Control Techniques," Journal of Aircraft, Vol. 31, No. 3, 1994, pp. 713-719.
    • (1994) Journal of Aircraft , vol.31 , Issue.3 , pp. 713-719
    • Nitzsche, F.1
  • 9
    • 0005823263 scopus 로고
    • Review of dynamic inflow modeling for rotorcraft flight dynamics
    • Gaonkar, G. H., and Peters, D. A., "Review of Dynamic Inflow Modeling for Rotorcraft Flight Dynamics," Vertica, Vol. 12, No. 3, 1988, pp. 213-242.
    • (1988) Vertica , vol.12 , Issue.3 , pp. 213-242
    • Gaonkar, G.H.1    Peters, D.A.2
  • 10
    • 0029272529 scopus 로고
    • Finite-state induced flow models, part II: Three-dimensional rotor disk
    • Peters, D. A., and He, C. J., "Finite-State Induced Flow Models, Part II: Three-Dimensional Rotor Disk," Journal of Aircraft, Vol. 32, No. 2, 1995, pp. 323-333.
    • (1995) Journal of Aircraft , vol.32 , Issue.2 , pp. 323-333
    • Peters, D.A.1    He, C.J.2
  • 12
    • 0043219992 scopus 로고
    • Boundary integral equation methods for aerodynamics
    • edited by S. N. Atluri, Progress in Astronautics and Aeronautics, AIAA, New York
    • Morino, L., and Gennaretti, M., "Boundary Integral Equation Methods for Aerodynamics," Computational Nonlinear Mechanics in Aerospace Engineering, edited by S. N. Atluri, Progress in Astronautics and Aeronautics, Vol. 146, AIAA, New York, 1992, pp. 279-320.
    • (1992) Computational Nonlinear Mechanics in Aerospace Engineering , vol.146 , pp. 279-320
    • Morino, L.1    Gennaretti, M.2
  • 13
    • 0031555839 scopus 로고    scopus 로고
    • A unified boundary integral methodology for aerodynamics and aeroacoustics of rotors
    • Gennaretti, M., Luceri, L., and Morino, L., "A Unified Boundary Integral Methodology for Aerodynamics and Aeroacoustics of Rotors," Journal of Sound and Vibration, Vol. 200, No. 4, 1997, pp. 467-489.
    • (1997) Journal of Sound and Vibration , vol.200 , Issue.4 , pp. 467-489
    • Gennaretti, M.1    Luceri, L.2    Morino, L.3
  • 14
    • 0020098320 scopus 로고
    • Design for the active flutter suppression and gust alleviation using state-space aeroelastic modeling
    • Karpel, M., "Design for the Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling," Journal of Aircraft, Vol. 19, No. 3, 1982, pp. 221-227.
    • (1982) Journal of Aircraft , vol.19 , Issue.3 , pp. 221-227
    • Karpel, M.1
  • 15
    • 0026257294 scopus 로고
    • Application of aeroservoelastic modeling using minimum-state unsteady aerodynamic approximations
    • Hoadley, S. T., and Karpel, M., "Application of Aeroservoelastic Modeling Using Minimum-State Unsteady Aerodynamic Approximations," Journal of Guidance, Control, and Dynamics, Vol. 14, No. 6, 1991, pp. 1267-1276.
    • (1991) Journal of Guidance, Control, and Dynamics , vol.14 , Issue.6 , pp. 1267-1276
    • Hoadley, S.T.1    Karpel, M.2
  • 16
    • 0029278505 scopus 로고
    • Matrix fraction approach for finite-state aerodynamic modeling
    • Morino, L., Mastroddi, F., De Troia, R., Ghiringhelli, G. L., and Mantegazza, P., "Matrix Fraction Approach for Finite-State Aerodynamic Modeling," AIM Journal, Vol. 33, No. 4, 1995, pp. 703-711.
    • (1995) AIM Journal , vol.33 , Issue.4 , pp. 703-711
    • Morino, L.1    Mastroddi, F.2    De Troia, R.3    Ghiringhelli, G.L.4    Mantegazza, P.5
  • 17
    • 0032669102 scopus 로고    scopus 로고
    • Finite-state aerodynamic modelling for gust load alleviation of wing-tail configurations
    • Gennaretti, M., and Ponzi, C., "Finite-State Aerodynamic Modelling for Gust Load Alleviation of Wing-Tail Configurations," Aeronautical Journal, Vol. 103, No. 1021, 1999, pp. 147-158.
    • (1999) Aeronautical Journal , vol.103 , Issue.1021 , pp. 147-158
    • Gennaretti, M.1    Ponzi, C.2
  • 18
    • 2342510183 scopus 로고    scopus 로고
    • Flap-lag rotor dynamics and aeroelastic stability using finite-state aerodynamics
    • Association Aéronautique et Astronautique de France, Marseilles, France, Sept.
    • Gennaretti, M., and Lisandrin, P., "Flap-Lag Rotor Dynamics and Aeroelastic Stability Using Finite-State Aerodynamics," Proceedings of the 24th European Rotorcraft Forum, Association Aéronautique et Astronautique de France, Marseilles, France, Sept. 1998, pp. DY.01.1-DY.01.11.
    • (1998) Proceedings of the 24th European Rotorcraft Forum
    • Gennaretti, M.1    Lisandrin, P.2
  • 19
    • 0042973877 scopus 로고    scopus 로고
    • Aeroacoustoelasticity in state-space format using CHIEF regularization
    • Gennaretti, M., and Iemma, U., "Aeroacoustoelasticity in State-Space Format Using CHIEF regularization," Journal of Fluids and Structures, Vol. 17, No. 7, 2003, pp. 983-999.
    • (2003) Journal of Fluids and Structures , vol.17 , Issue.7 , pp. 983-999
    • Gennaretti, M.1    Iemma, U.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.