-
1
-
-
0003803711
-
-
AIAA Education Series, AIAA, Washington, DC
-
Bielawa, R. L., Rotary Wing Structural Dynamics and Aeroelasticity, AIAA Education Series, AIAA, Washington, DC, 1992, p. 484.
-
(1992)
Rotary Wing Structural Dynamics and Aeroelasticity
, pp. 484
-
-
Bielawa, R.L.1
-
4
-
-
0020876814
-
Considerations in the estimation of full-scale rotor performance from model rotor test data
-
American Helicopter Society, MO, May
-
Keys, C. N., McVeigh, M. A., Dadone, L., and McHugh, F. J., "Considerations in the Estimation of Full-Scale Rotor Performance from Model Rotor Test Data," American Helicopter Society, Presented at the 39th Annual Forum of the AHS St. Louis, MO, May 1983, pp. 34-43.
-
(1983)
39th Annual Forum of the AHS St. Louis
, pp. 34-43
-
-
Keys, C.N.1
McVeigh, M.A.2
Dadone, L.3
McHugh, F.J.4
-
5
-
-
85037793522
-
Reynolds number influences on the aerodynamic performance of model-scale rotor blades
-
American Helicopter Society, Williamsburg, VA, Nov.
-
Bingham, G. J., and Kelley, H. L., "Reynolds Number Influences on the Aerodynamic Performance of Model-Scale Rotor Blades," American Helicopter Society, Presented at the AHS National Specialists Meeting on Helicopter Test Technology, Williamsburg, VA, Nov. 1984.
-
(1984)
AHS National Specialists Meeting on Helicopter Test Technology
-
-
Bingham, G.J.1
Kelley, H.L.2
-
6
-
-
0343821348
-
-
NASA TM-86440
-
Mantay, W. R., Yeager, W. T., Jr., Hamouda, M.-N., Cramer, R. G., Jr., and Langsten, C. W., "Aeroelastic Model Helicopter Rotor Testing in the Langley TDT," NASA TM-86440, 1985; also U.S. Army Aviation Systems Command, TM 85-B-5, 1985.
-
(1985)
Aeroelastic Model Helicopter Rotor Testing in the Langley TDT
-
-
Mantay, W.R.1
Yeager W.T., Jr.2
Hamouda, M.-N.3
Cramer R.G., Jr.4
Langsten, C.W.5
-
7
-
-
85037800977
-
-
TM 85-B-5
-
Mantay, W. R., Yeager, W. T., Jr., Hamouda, M.-N., Cramer, R. G., Jr., and Langsten, C. W., "Aeroelastic Model Helicopter Rotor Testing in the Langley TDT," NASA TM-86440, 1985; also U.S. Army Aviation Systems Command, TM 85-B-5, 1985.
-
(1985)
U.S. Army Aviation Systems Command
-
-
-
9
-
-
0003936844
-
-
PJS, Peoria, IL
-
Prouty, R. W., Helicopter Aerodynamics, PJS, Peoria, IL, 1985, p. 93.
-
(1985)
Helicopter Aerodynamics
, pp. 93
-
-
Prouty, R.W.1
-
10
-
-
0343821321
-
-
NASA TM 4183
-
Singleton, J. D., Yeager, W. T., Jr., and Wilbur, M. L., "Performance Data from a Wind-Tunnel Test of Two Main-Rotor Blade Designs for a Utility-Class Helicopter," NASA TM 4183, 1990; also U.S. Army Aviation Systems Command, TM 90-B-004, June 1990.
-
(1990)
Performance Data from a Wind-Tunnel Test of Two Main-Rotor Blade Designs for a Utility-Class Helicopter
-
-
Singleton, J.D.1
Yeager W.T., Jr.2
Wilbur, M.L.3
-
11
-
-
85037801040
-
-
TM 90-B-004, June
-
Singleton, J. D., Yeager, W. T., Jr., and Wilbur, M. L., "Performance Data from a Wind-Tunnel Test of Two Main-Rotor Blade Designs for a Utility-Class Helicopter," NASA TM 4183, 1990; also U.S. Army Aviation Systems Command, TM 90-B-004, June 1990.
-
(1990)
U.S. Army Aviation Systems Command
-
-
-
13
-
-
0343385675
-
-
NASA TP-1701, 1980; also U.S. Army Aviation Research and Development Command (AVRADCOM), TR 80-B-5
-
Noonan, K. W., and Bingham, G. J., "Aerodynamic Characteristics of Three Helicopter Rotor Airfoil Sections at Reynolds Numbers from Model Scale to Full Scale at Mach Numbers from 0.35 to 0.90," NASA TP-1701, 1980; also U.S. Army Aviation Research and Development Command (AVRADCOM), TR 80-B-5, 1980.
-
(1980)
Aerodynamic Characteristics of Three Helicopter Rotor Airfoil Sections at Reynolds Numbers from Model Scale to Full Scale at Mach Numbers from 0.35 to 0.90
-
-
Noonan, K.W.1
Bingham, G.J.2
-
14
-
-
0004232657
-
-
Frederick Ungar, New York
-
Gessow, A., and Myers, G. C., Aerodynamics of the Helicopter, Frederick Ungar, New York, 1952, pp. 47-116.
-
(1952)
Aerodynamics of the Helicopter
, pp. 47-116
-
-
Gessow, A.1
Myers, G.C.2
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