메뉴 건너뛰기




Volumn 63, Issue 1, 2018, Pages

Wind tunnel test of the SMART active flap rotor

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; AERODYNAMICS; HELICOPTER ROTORS; INTELLIGENT MATERIALS; NASA; SOFTWARE TESTING; WIND STRESS;

EID: 85013324653     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/JAHS.63.012002     Document Type: Conference Paper
Times cited : (91)

References (41)
  • 2
    • 0010021160 scopus 로고
    • Higher harmonic control: Flight tests of an experimental system on sa 349 research gazelle
    • Washington DC June 2-5
    • 2Polychroniadis, M., and Achache, M., "Higher Harmonic Control: Flight Tests of an Experimental System on SA 349 Research Gazelle, " American Helicopter Society 42nd Annual Forum Proceedings, Washington, DC, June 2-5, 1986.
    • (1986) American Helicopter Society 42nd Annual Forum Proceedings
    • Polychroniadis, M.1    Achache, M.2
  • 4
    • 4143126551 scopus 로고    scopus 로고
    • Reduction of bvinoise on ground-in-flight evaluation of closed-loop controller
    • Bristol, UK September 17-20
    • 4Bebesel, M., Roth, D., and Pongratz, R., "Reduction of BVINoise on Ground-In-Flight Evaluation of Closed-Loop Controller, " Proceedings of the 28th European Rotorcraft Forum, Bristol, UK, September 17-20, 2002.
    • (2002) Proceedings of the 28th European Rotorcraft Forum
    • Bebesel, M.1    Roth, D.2    Pongratz, R.3
  • 5
    • 33745536067 scopus 로고    scopus 로고
    • Advanced vibration reduction by ibc technology
    • Marseilles, France September 14-16
    • 5Roth, D., "Advanced Vibration Reduction by IBC Technology, " Proceedings of the 30th European Rotorcraft Forum, Marseilles, France, September 14-16, 2004.
    • (2004) Proceedings of the 30th European Rotorcraft Forum
    • Roth, D.1
  • 6
    • 4143139712 scopus 로고    scopus 로고
    • Open loop flight test results and closed loop status of the ibc system on the ch-53g helicopter
    • Phoenix, AZ May 6-8
    • 6Kessler, C., Fuerst, D., and Arnold, U. T. P., "Open Loop Flight Test Results and Closed Loop Status of the IBC System on the CH-53G Helicopter, " American Helicopter Society 59th Annual Forum Proceedings, Phoenix, AZ, May 6-8, 2003.
    • (2003) American Helicopter Society 59th Annual Forum Proceedings
    • Kessler, C.1    Fuerst, D.2    Arnold, U.T.P.3
  • 7
    • 4143067965 scopus 로고    scopus 로고
    • Recent ibc flight test results from the ch-53g helicopter
    • Friedrichshafen, Germany September 16-18
    • 7Arnold, U. T. P., "Recent IBC Flight Test Results from the CH-53G Helicopter, " Proceedings of the 29th European Rotorcraft Forum, Friedrichshafen, Germany, September 16-18, 2003.
    • (2003) Proceedings of the 29th European Rotorcraft Forum
    • Arnold, U.T.P.1
  • 8
    • 33748474381 scopus 로고    scopus 로고
    • Trailing edge flaps for active rotor control-aeroelastic characteristics of the adasys rotor system
    • Phoenix, AZ May 9-11
    • 8Dieterich, O., Enenkl, B., and Roth, D., "Trailing Edge Flaps for Active Rotor Control-Aeroelastic Characteristics of the ADASYS Rotor System, " American Helicopter Society 62nd Annual Forum Proceedings, Phoenix, AZ, May 9-11, 2006.
    • (2006) American Helicopter Society 62nd Annual Forum Proceedings
    • Dieterich, O.1    Enenkl, B.2    Roth, D.3
  • 11
    • 0031651091 scopus 로고    scopus 로고
    • Small-scale rotor experiments with on-blade elevons to reduce blade vibratory loads in forward flight
    • Washington DC May 20-22
    • 11Fulton, M.V., and Ormiston, R. A., "Small-Scale Rotor Experiments with On-Blade Elevons to Reduce Blade Vibratory Loads in Forward Flight, " American Helicopter Society 54th Annual Forum Proceedings, Washington, DC, May 20-22, 1998.
    • (1998) American Helicopter Society 54th Annual Forum Proceedings
    • Fulton, M.V.1    Ormiston, R.A.2
  • 12
    • 0033666349 scopus 로고    scopus 로고
    • Closed-loop vibration control experiments on a rotor with blade mounted actuation
    • Atlanta, GA, April 3-6, 2000
    • 12Prechtl, E., and Hall, S. R., "Closed-Loop Vibration Control Experiments on a Rotor with Blade Mounted Actuation, " AIAA 2000-1714, Proceedings of the 41st AIAA SDMConference, Atlanta, GA, April 3-6, 2000.
    • AIAA 2000-1714 Proceedings of the 41st AIAA SDMConference
    • Prechtl, E.1    Hall, S.R.2
  • 20
    • 84911191300 scopus 로고    scopus 로고
    • On-blade control of rotor vibration, noise, and performance: Just around the corner?
    • 20Friedmann, P. P., "On-Blade Control of Rotor Vibration, Noise, and Performance: Just around the Corner?" Journal of the American Helicopter Society, 59, 041001 (2014).
    • (2014) Journal of the American Helicopter Society , vol.59 , pp. 041001
    • Friedmann, P.P.1
  • 23
  • 25
    • 14144249428 scopus 로고    scopus 로고
    • Rotorcraft vibration reduction and noise prediction using a unified aeroelastic response simulation
    • January
    • 25Patt, D., Liu, L., and Friedmann, P. P., "Rotorcraft Vibration Reduction and Noise Prediction Using a Unified Aeroelastic Response Simulation, " Journal of the American Helicopter Society, Vol. 50, (1), January 2005, pp. 95-106.
    • (2005) Journal of the American Helicopter Society , vol.50 , Issue.1 , pp. 95-106
    • Patt, D.1    Liu, L.2    Friedmann, P.P.3
  • 26
    • 33748453872 scopus 로고    scopus 로고
    • Simultaneous vibration reduction and performance enhancement in rotorcraft using actively controlled flaps
    • Phoenix, AZ May 9-11
    • 26Liu, L., Friedmann, P. P., Kim, I., and Bernstein, D. S., "Simultaneous Vibration Reduction and Performance Enhancement in Rotorcraft Using Actively Controlled Flaps, " American Helicopter Society 62nd Annual Forum Proceedings, Phoenix, AZ, May 9-11, 2006.
    • (2006) American Helicopter Society 62nd Annual Forum Proceedings
    • Liu, L.1    Friedmann, P.P.2    Kim, I.3    Bernstein, D.S.4
  • 27
    • 50249083308 scopus 로고    scopus 로고
    • Prediction and validation of loads on bearingless rotorsusing a coupled cfd-csdmethodology
    • Montreal, Canada April 29-May 1
    • 27Ananthan, S., and Baeder, J. D., "Prediction and Validation of Loads on Bearingless RotorsUsing a Coupled CFD-CSDMethodology, " American Helicopter Society 64th Annual Forum Proceedings, Montreal, Canada, April 29-May 1, 2008.
    • (2008) American Helicopter Society 64th Annual Forum Proceedings
    • Ananthan, S.1    Baeder, J.D.2
  • 31
    • 0029712784 scopus 로고    scopus 로고
    • Aeromechanic considerations in the design of a rotor with smart material actuated trailing edge flaps
    • Washington DC June 4-6
    • 31Straub, F. K., and Hassan, A. A., "Aeromechanic Considerations in the Design of a Rotor with Smart Material Actuated Trailing Edge Flaps, " American Helicopter Society 52nd Annual Forum Proceedings, Washington DC, June 4-6, 1996.
    • (1996) American Helicopter Society 52nd Annual Forum Proceedings
    • Straub, F.K.1    Hassan, A.A.2
  • 34
    • 70350479095 scopus 로고
    • Full-scale wind tunnel test of the mcdonnell douglas five-bladed advanced bearingless rotor: Performance, stability, loads, control power, vibration and HHC Data
    • San Francisco, CA January 19-21
    • 34Jacklin, S. A., Lau, B. H., Nguyen, K. Q., Smith, R. L., and McNulty, M., "Full-Scale Wind Tunnel Test of the McDonnell Douglas Five-Bladed Advanced Bearingless Rotor: Performance, Stability, Loads, Control Power, Vibration and HHC Data, " Proceedings of the American Helicopter Society Aeromechanics Specialists' Conference, San Francisco, CA, January 19-21, 1994.
    • (1994) Proceedings of the American Helicopter Society Aeromechanics Specialists' Conference
    • Jacklin, S.A.1    Lau, B.H.2    Nguyen, K.Q.3    Smith, R.L.4    McNulty, M.5
  • 36
    • 70350448224 scopus 로고    scopus 로고
    • Reduced in-plane, low frequency noise of an active flap rotor
    • TX Maya, lso Journal of the American Helicopter Society 59 022002 2014
    • 36Sim, B. W., JanakiRam, R. D., Barbely, N. L., and Solis, E., "Reduced In-Plane, Low Frequency Noise of an Active Flap Rotor, " American Helicopter Society 65th Annual Forum Proceedings, TX, May 2009; also Journal of the American Helicopter Society, 59, 022002 (2014).
    • (2009) American Helicopter Society 65th Annual Forum Proceedings
    • Sim, B.W.1    JanakiRam, R.D.2    Barbely, N.L.3    Solis, E.4
  • 38
    • 0019685340 scopus 로고
    • A unified approach to the optimal design of adaptive and gain scheduled controllers to achieve minimum helicopter vibrations
    • New Orleans, LA May 17-20
    • 38Molusis, J. A., Hammond, C. E., and Cline, J. H., "A Unified Approach to the Optimal Design of Adaptive and Gain Scheduled Controllers to Achieve Minimum Helicopter Vibrations, " American Helicopter Society 37th Annual Forum Proceedings, New Orleans, LA, May 17-20, 1981.
    • (1981) American Helicopter Society 37th Annual Forum Proceedings
    • Molusis, J.A.1    Hammond, C.E.2    Cline, J.H.3
  • 39
    • 0035389792 scopus 로고    scopus 로고
    • Comprehensive modeling of rotors with trailing edge flaps
    • July
    • 39Straub, F. K., and Charles, B. D., "Comprehensive Modeling of Rotors with Trailing Edge Flaps, " Journal of the American Helicopter Society, Vol. 46, (3), July 2001, pp. 192-199.
    • (2001) Journal of the American Helicopter Society , vol.46 , Issue.3 , pp. 192-199
    • Straub, F.K.1    Charles, B.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.