메뉴 건너뛰기




Volumn 1, Issue , 2005, Pages 492-517

A computational study of helicopter rotor wakes and noise generated during transient maneuvers

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT MANEUVERS; ROLL-REVERSAL MAEUVERS; ROTOR BLADES;

EID: 33644671252     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (32)
  • 4
    • 33644690588 scopus 로고    scopus 로고
    • Predictions of transient wake aerodynamics in response to time-dependent pilot control inputs
    • Phoenix, AZ, May 6-9
    • Ananthan, S., and Leishman, J. G., "Predictions of Transient Wake Aerodynamics in Response to Time-Dependent Pilot Control Inputs," American Helicopter Society 59th Annual Forum Proceedings, Phoenix, AZ, May 6-9 2003.
    • (2003) American Helicopter Society 59th Annual Forum Proceedings
    • Ananthan, S.1    Leishman, J.G.2
  • 5
    • 2942587191 scopus 로고
    • A balsa-dust technique for air-flow visualization and its application to flow through model helicopter rotors in static thrust
    • November
    • Taylor, M. K., "A Balsa-Dust Technique for Air-Flow Visualization and its Application to Flow through Model Helicopter Rotors in Static Thrust," NACA TN-2220, November, 1950.
    • (1950) NACA TN-2220
    • Taylor, M.K.1
  • 6
    • 0012661340 scopus 로고
    • Effect of a rapid blade-pitch increase on the thrust and induced-velocity response of a full-scale helicopter rotor
    • November
    • Carpenter, P. J., and Friedovich, B., "Effect of A Rapid Blade-Pitch Increase on the Thrust and Induced-Velocity Response of a Full-Scale Helicopter Rotor," NACA TN-3044, November 1953.
    • (1953) NACA TN-3044
    • Carpenter, P.J.1    Friedovich, B.2
  • 7
    • 4143075875 scopus 로고    scopus 로고
    • Apparent mass effects on a stiff-hinged rotor model after rapid cyclic and/or collective inputs - A flow visualization study
    • Moscow, Russia, September 11-14
    • Jessurun, K. P., Pavel, M. D., and Toet, S., "Apparent Mass Effects on a Stiff-Hinged Rotor Model after Rapid Cyclic and/or Collective Inputs - A Flow Visualization Study," 27th European Rotorcraft Forum, Moscow, Russia, September 11-14, 2001.
    • (2001) 27th European Rotorcraft Forum
    • Jessurun, K.P.1    Pavel, M.D.2    Toet, S.3
  • 9
    • 0029344665 scopus 로고
    • A new model for rotor dynamics during pitch and roll of a hovering helicopter
    • Rosen, A., and Isser, A., "A New Model for Rotor Dynamics During Pitch and Roll of a Hovering Helicopter," Journal of the American Helicopter Society, Vol. 40 (3), 1995, pp. 17-28.
    • (1995) Journal of the American Helicopter Society , vol.40 , Issue.3 , pp. 17-28
    • Rosen, A.1    Isser, A.2
  • 12
    • 33644682417 scopus 로고    scopus 로고
    • Prediction of the off-axis response to cyclic pitch using a maneuvering free wake model
    • Rome, Italy, September
    • Theodore, C., and Celi, R., "Prediction of the Off-Axis Response to Cyclic Pitch Using a Maneuvering Free Wake Model," 25th European Rotorcraft Forum, Rome, Italy, September, 1999.
    • (1999) 25th European Rotorcraft Forum
    • Theodore, C.1    Celi, R.2
  • 15
    • 85086613330 scopus 로고    scopus 로고
    • Noise prediction for maneuvering rotorcraft
    • Paper No. AIAA 2000-2031, Lahaina, HI, June 12-14
    • Brentner, K. S., and Jones, H. E., "Noise Prediction for Maneuvering Rotorcraft," Paper No. AIAA 2000-2031, 6th AIAA/CEAS Aeroacoustics Conference, Lahaina, HI, June 12-14 2000.
    • (2000) 6th AIAA/CEAS Aeroacoustics Conference
    • Brentner, K.S.1    Jones, H.E.2
  • 19
    • 23844515893 scopus 로고
    • UH-60A BLACK HAWK engineering simulation program: Volume I - Mathematical model
    • USAAVSCOM TR 89-A-001, September
    • Howlett, J., "UH-60A BLACK HAWK Engineering Simulation Program: Volume I - Mathematical Model," NASA CR-177542, USAAVSCOM TR 89-A-001, September, 1989.
    • (1989) NASA CR-177542
    • Howlett, J.1
  • 20
    • 0036757422 scopus 로고    scopus 로고
    • Free-vortex filament methods for the analysis of helicopter rotor wakes
    • September-October
    • Leishman, J. G., Bhagwat, M. J., and Bagai, A., "Free-Vortex Filament Methods for the Analysis of Helicopter Rotor Wakes," Journal of Aircraft, Vol. 39 (5), September-October 2002, pp. 759-775.
    • (2002) Journal of Aircraft , vol.39 , Issue.5 , pp. 759-775
    • Leishman, J.G.1    Bhagwat, M.J.2    Bagai, A.3
  • 21
    • 85041150744 scopus 로고
    • Cambridge University Press, Cambridge, UK
    • Saffman, P. G., Vortex Dynamics, Cambridge University Press, Cambridge, UK, 1992.
    • (1992) Vortex Dynamics
    • Saffman, P.G.1
  • 23
    • 0035119640 scopus 로고    scopus 로고
    • Stability, consistency and convergence of time-marching free-vortex rotor wake algorithms
    • January
    • Bhagwat, M. J., and Leishman, J. G., "Stability, Consistency and Convergence of Time-Marching Free-Vortex Rotor Wake Algorithms," Journal of the American Helicopter Society, Vol. 46 (1), January 2001, pp. 59-71.
    • (2001) Journal of the American Helicopter Society , vol.46 , Issue.1 , pp. 59-71
    • Bhagwat, M.J.1    Leishman, J.G.2
  • 24
    • 34250860894 scopus 로고    scopus 로고
    • Role of filament strain in the free-vortex modeling of rotor wakes
    • April
    • Ananthan, S., and Leishman, J. G., "Role of Filament Strain in the Free-Vortex Modeling of Rotor Wakes," Journal of the American Helicopter Society, Vol. 49 (2), April 2004, pp. 176-191.
    • (2004) Journal of the American Helicopter Society , vol.49 , Issue.2 , pp. 176-191
    • Ananthan, S.1    Leishman, J.G.2
  • 26
    • 0003198192 scopus 로고
    • The lift distribution of swept-back wings
    • Weissinger, J., "The Lift Distribution of Swept-Back Wings," NACA TM 1120, 1947.
    • (1947) NACA TM , vol.1120
    • Weissinger, J.1
  • 27
    • 0029703891 scopus 로고    scopus 로고
    • Aeroacoustics of 2-D and 3-D blade vortex interaction using the indicial method
    • Washington, DC, June 4-6
    • Leishman, J. G., "Aeroacoustics of 2-D and 3-D Blade Vortex Interaction Using the Indicial Method," American Helicopter Society 52nd Annual Forum Proceedings, Washington, DC, June 4-6, 1996.
    • (1996) American Helicopter Society 52nd Annual Forum Proceedings
    • Leishman, J.G.1
  • 28
    • 0030247268 scopus 로고    scopus 로고
    • Unsteady aerodynamics of flapped airfoil in subsonic flow by indicial concepts
    • September-October
    • Hariharan, N., and Leishman, J. G., "Unsteady Aerodynamics of Flapped Airfoil in Subsonic Flow by Indicial Concepts," Journal of Aircraft, Vol. 33 (5), September-October 1996, pp. 855-867.
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 855-867
    • Hariharan, N.1    Leishman, J.G.2
  • 29
    • 0021076378 scopus 로고
    • The prediction of helicopter rotor discrete frequency noise
    • Farassat, F., and Succi, G. P., "The Prediction of Helicopter Rotor Discrete Frequency Noise," Vertica, Vol. 7 (4), 1983, pp. 309-320.
    • (1983) Vertica , vol.7 , Issue.4 , pp. 309-320
    • Farassat, F.1    Succi, G.P.2
  • 30
    • 0000950129 scopus 로고    scopus 로고
    • An analytical comparison of the acoustic analogy and kirchhoff formulation for moving surfaces
    • Brentner, K. S., and Farassat, F., "An Analytical Comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces," AIAA Journal, Vol. 36 (8), 1998, pp. 1379-1386.
    • (1998) AIAA Journal , vol.36 , Issue.8 , pp. 1379-1386
    • Brentner, K.S.1    Farassat, F.2
  • 31
    • 33644683445 scopus 로고
    • Kirchoff code - A versatile CAA tool
    • Advanced Rotorcraft Technology, June
    • "Kirchoff Code - a Versatile CAA Tool," NASA SBIR phase I final report, Advanced Rotorcraft Technology, June, 1995.
    • (1995) NASA SBIR Phase i Final Report


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.