-
4
-
-
17944392632
-
Wind Tunnel Test Results of a Full-Scale Multicyclic Controllable Twist Rotor
-
Washington, D.C., May
-
McCloud III, J. L. and Weisbrich, A. L., "Wind Tunnel Test Results of a Full-Scale Multicyclic Controllable Twist Rotor," Proceedings of the 34th Annual National Forum of the American Helicopter Society, Washington, D.C., May 1978.
-
(1978)
Proceedings of the 34th Annual National Forum of the American Helicopter Society
-
-
McCloud III, J.L.1
Weisbrich, A.L.2
-
5
-
-
0023437632
-
Use of Piezoelectric Actuators as Elements of Intelligent Structures
-
Oct
-
Crawley, E. F. and de Luis, J., "Use of Piezoelectric Actuators as Elements of Intelligent Structures," AIAA Journal, Vol. 25, (10), pp. 1373-1385, Oct 1987.
-
(1987)
AIAA Journal
, vol.25
, Issue.10
, pp. 1373-1385
-
-
Crawley, E.F.1
De Luis, J.2
-
6
-
-
0025258095
-
Piezoelectric Actuators for Helicopter Rotor Control
-
Long Beach, CA, Apr Paper AIAA-90-1076-CP
-
Spangler, R. L. and Hall, S. R., "Piezoelectric Actuators for Helicopter Rotor Control," Proceedings of the 31st AIAA Structures, Structural Dynamics and Materials Conference, pp. 1589-1599, Long Beach, CA, Apr 1990. Paper AIAA-90-1076-CP.
-
(1990)
Proceedings of the 31st AIAA Structures, Structural Dynamics and Materials Conference
, pp. 1589-1599
-
-
Spangler, R.L.1
Hall, S.R.2
-
7
-
-
85075986471
-
Terfenol-D Driven Flaps for Helicopter Vibration Reduction
-
Albuquerque, NM
-
Fenn, R. C., Downer, J. R., Bushko, D. A., Gondhalekar, V, and Ham, N. D., "Terfenol-D Driven Flaps for Helicopter Vibration Reduction," Proceedings of the SPIE Conference on Smart Structures and Intelligent Systems, pp. 225-237, Albuquerque, NM, 1993.
-
(1993)
Proceedings of the SPIE Conference on Smart Structures and Intelligent Systems
, pp. 225-237
-
-
Fenn, R.C.1
Downer, J.R.2
Bushko, D.A.3
Gondhalekar, V.4
Ham, N.D.5
-
8
-
-
85008292148
-
A Feasibility Study to Build a Smart Rotor: Trailing Edge Flap Actuation
-
Albuquerque, NM
-
Samak, D. K. and Chopra, I., "A Feasibility Study to Build a Smart Rotor: Trailing Edge Flap Actuation," Proceedings of the SPIE Conference on Smart Structures and Intelligent Systems, pp. 407-418, Albuquerque, NM, 1993.
-
(1993)
Proceedings of the SPIE Conference on Smart Structures and Intelligent Systems
, pp. 407-418
-
-
Samak, D.K.1
Chopra, I.2
-
9
-
-
0002332181
-
Design and Testing of a Helicopter Rotor Model with Smart Trailing Edge Flaps
-
Apr AIAA-94-1767-CP
-
Walz, C. and Chopra, I., "Design and Testing of a Helicopter Rotor Model with Smart Trailing Edge Flaps," Proceedings of the 35th Structures, Structural Dynamics and Materials Conference, Adaptive Structures Forum, Apr 1994. AIAA-94-1767-CP.
-
(1994)
Proceedings of the 35th Structures, Structural Dynamics and Materials Conference, Adaptive Structures Forum
-
-
Walz, C.1
Chopra, I.2
-
11
-
-
0002828953
-
Design, Validation, and Test of a Model Rotor with Tip Mounted Active Flaps
-
Washington, D.C., May
-
Dawson, S. and Straub, F., "Design, Validation, and Test of a Model Rotor with Tip Mounted Active Flaps," Proceedings of the 50th Annual Forum of the American Helicopter Society, Washington, D.C., May 1994.
-
(1994)
Proceedings of the 50th Annual Forum of the American Helicopter Society
-
-
Dawson, S.1
Straub, F.2
-
15
-
-
3042652312
-
Blade-Mounted Flap Control for BVI Noise Reduction Proof of Concept Test
-
Jul
-
Dawson, S. Hassan, A., Straub, F., and Tadghighi, H., "BladeMounted Flap Control for BVI Noise Reduction Proof of Concept Test," NASA Contractor Report 195078, Jul 1995.
-
(1995)
NASA Contractor Report 195078
-
-
Dawson, S.1
Hassan, A.2
Straub, F.3
Tadghighi, H.4
-
16
-
-
0004974797
-
Vibration Reduction in Helicopter Rotors Using an Active Control Surface Located on the Blade
-
Dallas, TX Apr AIAA paper 92-2451
-
Millott, T. A. and Friedmann, P. P., "Vibration Reduction in Helicopter Rotors Using an Active Control Surface Located on the Blade," Proceedings of the 33rd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, Dallas, TX Apr 1992. AIAA paper 92-2451.
-
(1992)
Proceedings of the 33rd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference
-
-
Millott, T.A.1
Friedmann, P.P.2
-
17
-
-
0005188729
-
The Practical Implementation of an Actively Controlled Flap to Reduce Vibrations in Helicopter Rotors
-
St. Louis, May
-
Millott, T. A. and Friedmann, P. P., "The Practical Implementation of an Actively Controlled Flap to Reduce Vibrations in Helicopter Rotors," Proceedings of the 49th Annual Forum of the American Helicopter Society, pp. 1079-1092, St. Louis, May 1993.
-
(1993)
Proceedings of the 49th Annual Forum of the American Helicopter Society
, pp. 1079-1092
-
-
Millott, T.A.1
Friedmann, P.P.2
-
18
-
-
0028695920
-
Vibration Reduction in Hingeless Rotors Using an Actively Controlled Trailing Edge Flap: Implementation and Time Domain Simulation
-
Apr AIAA-94-1306-CP
-
Millott, T. A. and Friedmann, P. P., "Vibration Reduction in Hingeless Rotors Using an Actively Controlled Trailing Edge Flap: Implementation and Time Domain Simulation," Proceedings of the 35th Structures, Structural Dynamics and Materials Conference, Adaptive Structures Forum, Apr 1994. AIAA-94-1306-CP.
-
(1994)
Proceedings of the 35th Structures, Structural Dynamics and Materials Conference, Adaptive Structures Forum
-
-
Millott, T.A.1
Friedmann, P.P.2
-
19
-
-
0003982040
-
-
Contractor Report 4611, NASA, Jun
-
Millott, T. A. and Friedmann, P. P., "Vibration Reduction in Helicopter Rotors Using an Actively Controlled Partial Span Trailing Edge Flap Located on the Blade," Contractor Report 4611, NASA, Jun 1994.
-
(1994)
Vibration Reduction in Helicopter Rotors Using An Actively Controlled Partial Span Trailing Edge Flap Located on the Blade
-
-
Millott, T.A.1
Friedmann, P.P.2
-
20
-
-
0029212635
-
Helicopter Vibration Reduction with Trailing Edge Flaps
-
New Orleans, LA, Apr
-
Milgram, J. H. and Chopra, I., "Helicopter Vibration Reduction with Trailing Edge Flaps," Proceedings of the 36th AAIA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics, and Materials Conference, New Orleans, LA, Apr 1995.
-
(1995)
Proceedings of the 36th AAIA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics, and Materials Conference
-
-
Milgram, J.H.1
Chopra, I.2
-
21
-
-
11744288552
-
Helicopter Vibration Reduction with Trailing Edge Flaps
-
Stratford, CT, Oct
-
Milgram, J. H. and Chopra, I., "Helicopter Vibration Reduction with Trailing Edge Flaps," Proceedings of the American Helicopter Society Northeast Region Aeromechanics Speccialists Meeting, Stratford, CT, Oct 1995.
-
(1995)
Proceedings of the American Helicopter Society Northeast Region Aeromechanics Speccialists Meeting
-
-
Milgram, J.H.1
Chopra, I.2
-
22
-
-
0012471984
-
-
Technical Report UM-AERO 94-18, Center for Rotorcraft Education and Research, University of Maryland, College Park, MD, Jul
-
Bir, G., Chopra, L, et al. University of Maryland Advanced Rotor Code (UMARC) Theory Manual, Technical Report UM-AERO 94-18, Center for Rotorcraft Education and Research, University of Maryland, College Park, MD, Jul 1994.
-
(1994)
University of Maryland Advanced Rotor Code (UMARC) Theory Manual
-
-
Bir, G.1
Chopra, L.2
-
23
-
-
0029223007
-
Unsteady Aerodynamics of a Flapped Airfoil in Subsonic Flow by lndicial Concepts
-
New Orleans, LA, Apr
-
Hariharan, N. and Leishman, J. G., "Unsteady Aerodynamics of a Flapped Airfoil in Subsonic Flow by lndicial Concepts," Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, New Orleans, LA, Apr 1995.
-
(1995)
Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
-
-
Hariharan, N.1
Leishman, J.G.2
-
25
-
-
0006763249
-
-
Ph.D. thesis, University of Maryland, College Park, MD, Jan
-
Milgram, J. H. A Comprehensive Aeroelastic Analysis of Helicopter Main Rotors with Trailing Edge Flaps for Vibration Reduction, Ph.D. thesis, University of Maryland, College Park, MD, Jan 1997.
-
(1997)
A Comprehensive Aeroelastic Analysis of Helicopter Main Rotors with Trailing Edge Flaps for Vibration Reduction
-
-
Milgram, J.H.1
-
27
-
-
0029703945
-
A Comprehensive Rotorcraft Aeroelastic Analysis with Trailing Edge Flap Model: Validation with Experimental Data
-
Jun
-
Milgram, J. H., Chopra, L, and Straub, F., "A Comprehensive Rotorcraft Aeroelastic Analysis with Trailing Edge Flap Model: Validation with Experimental Data," Proceedings of the 52nd Annual Forum of the American Helicopter Society, Jun 1996
-
(1996)
Proceedings of the 52nd Annual Forum of the American Helicopter Society
-
-
Milgram, J.H.1
Chopra, L.2
Straub, F.3
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