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10
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28844456935
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Blade-vortex interaction noise characteristics of a full-scale active flap rotor
-
Grapevine, TX, May 27-29
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th Annual Forum of the AHS, Grapevine, TX, May 27-29, 2009
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(2009)
th Annual Forum of the AHS
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-
JanakiRam, R.D.1
Sim, B.W.2
Kitaplioglu, C.3
Straub, F.K.4
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68
-
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70350448224
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Reduced in-plane, low frequency noise of an active flap rotor
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Grapevine, TX, May 27-29
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th Annual Forum of the AHS, Grapevine, TX, May 27-29, 2009.
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(2009)
th Annual Forum of the AHS
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-
Sim, B.W.1
JanakiRam, R.D.2
Barbely, N.L.3
Solis, E.4
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69
-
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0343995306
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Development of a smart rotor
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Cernobbio, Italy, September 14-16
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th ERF, Cernobbio, Italy, September 14-16, 1993.
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(1993)
th ERF
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Chopra, I.1
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70
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2942557270
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The design evolution of an active materials rotor
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Washington, DC, May 9-11
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th Annual Forum of the AHS, Washington, DC, May 9-11, 2001.
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(2001)
th Annual Forum of the AHS
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Derham, R.1
Weems, D.2
Mathew, M.B.3
Bussom, R.4
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71
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4143108970
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A large-scale active twist rotor
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Baltimore, MD, June 7-10
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th Annual Forum of the AHS, Baltimore, MD, June 7-10, 2004.
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(2004)
th Annual Forum of the AHS
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Weems, D.B.1
Anderson, D.M.2
Mathew, M.B.3
Bussom, R.C.4
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72
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1242268607
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Vibration reduction testing of the NASA/ARMY/MIT active twist rotor
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Washington, DC, May 9-11
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th Annual Forum of the AHS, Washington, DC, May 9-11, 2001.
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(2001)
th Annual Forum of the AHS
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-
Wilbur, M.L.1
Mirick, P.H.2
Yaeger, W.T.3
Langston, C.W.4
Cesnik, C.E.S.5
Shin, S.6
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74
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77952340665
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Evolution of active twist rotor design at DLR
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Schaumburg, IL, April 7-10
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Monner, H.P., Opitz, S., Riemenschneider, J., Wierach, P.: Evolution of Active Twist Rotor Design at DLR, AIAA/ASME/AHS Adaptive Structures Conference, Schaumburg, IL, April 7-10, 2008.
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(2008)
AIAA/ASME/AHS Adaptive Structures Conference
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-
Monner, H.P.1
Opitz, S.2
Riemenschneider, J.3
Wierach, P.4
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76
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-
84921421819
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A new concept of active twist blade applied to main rotor of helicopter
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Evora, Portugal, RTO-MP-AVT-168, April 20-24
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des Rochettes, H.M., Joly, D., Buchaniek, L., Leconte P.: A New Concept of Active Twist Blade Applied to Main Rotor of Helicopter, RTO Applied Vehicle Technology Panel Symposium, Evora, Portugal, RTO-MP-AVT-168, April 20-24, 2009.
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(2009)
RTO Applied Vehicle Technology Panel Symposium
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Des Rochettes, H.M.1
Joly, D.2
Buchaniek, L.3
Leconte, P.4
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77
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77952341024
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Structural design and testing of active twist blades - A comparison
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Hamburg, Germany, September 22-24
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th ERF, Hamburg, Germany, September 22-24, 2009.
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(2009)
th ERF
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Riemenschneider, J.1
Opitz, S.2
Wierach, P.3
Des Rochettes, H.M.4
Buchaniek, L.5
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81
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0017268001
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Research in multicyclic and active control of rotary wings
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Kretz, M.: Research in Multicyclic and Active Control of Rotary Wings, Vertica, Vo. I, No. 2 pp. 95-105, 1976.
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Kretz, M.1
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82
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0020154729
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Individual blade control independent of a swashplate
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Guinn, K. F.: Individual Blade Control Independent of a Swashplate, Journal of the AHS, Vol. 27, No. 3, pp. 25-31, 1982.
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Journal of the AHS
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Guinn, K.F.1
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83
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84921409759
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Development of an integrated electrical swashplateless primary and individual blade control system
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Maastricht, The Netherlands, September 12-14
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nd ERF, Maastricht, The Netherlands, September 12-14, 2006.
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nd ERF
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Arnold, U.T.P.1
Fuerst, D.2
Neuheuser, T.3
Bartels, R.4
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84
-
-
78149330571
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Whirl test of a large scale high authority active flap rotor
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Phoenix, AZ, May 11-13
-
th Annual Forum of the AHS, Phoenix, AZ, May 11-13, 2010.
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(2010)
th Annual Forum of the AHS
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Lorber, P.F.1
O'Neil, J.J.2
Isabella, B.3
Andrews, J.4
Wong, J.5
Hein, B.6
Geiger, D.7
Wake, B.E.8
Jonsson, U.9
Sun, F.10
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86
-
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85048671797
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Helicopter horizontal tail incidence control to reduce rotor cyclic pitch and blade flapping
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Baltimore, MD, June 7-10, 004
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th Annual Forum of the AHS, Baltimore, MD, June 7-10, 004.
-
th Annual Forum of the AHS
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-
Ghandi, F.1
Sekula, M.2
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