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United States. Army Aviation Research and Technology Activi ...
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1

A method for determining spiral-bevel gear tooth geometry f..:

Handschuh, Robert F ; Litvin, F. L. (Faydor L.) ; United States. Army Aviation Research and Technology Activity. Propulsion Directorate.
http://hdl.handle.net/2027/uiug.30112106710947.  , 1991
Link: http://hdl.handle.net/20..
 
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2

The effects of structural flap-lag and pitch-lag coupling o..:

Bousman, William G. (William Giles) ; United States. Army Aviation Research and Technology Activity ; Ames Research Center
http://hdl.handle.net/2027/uiug.30112106709733.  , 1990
Link: http://hdl.handle.net/20..
 
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3

Experimental and analytical evaluation of efficiency of hel..:

Krantz, T. L. (Timothy L.) ; United States. Army Aviation Research and Technology Activity. Propulsion Directorate ; Lewis Research Center
http://hdl.handle.net/2027/uiug.30112106711267.  , 1990
Link: http://hdl.handle.net/20..
 
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4

Acoustic measurements from a rotor blade-vortex interaction..:

Martin, R. M. (Ruth McVoy), 1956- ; United States. Army Aviation Research and Technology Activity ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
http://hdl.handle.net/2027/uiug.30112106721829.  , 1988
Link: http://hdl.handle.net/20..
 
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5

Effect of planform taper on hover performance of an advance..:

Kelley, Henry L ; United States. Army Aviation Research and Technology Activity ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112018023447.  , 1987
Link: http://hdl.handle.net/20..
 
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6

Helicopter blade-vortex interaction locations : scale-model..:

Hoad, Danny R ; United States. Army Aviation Research and Technology Activity. Aerostructures Directorate
http://hdl.handle.net/2027/uiug.30112106613141.  , 1987
Link: http://hdl.handle.net/20..
 
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7

Vibration characteristics of OH-58A helicopter main rotor t..:

Lewicki, David G ; Coy, John J ; United States. Army Aviation Research and Technology Activity. Propulsion Directorate.
http://hdl.handle.net/2027/uiug.30112106605444.  , 1987
Link: http://hdl.handle.net/20..
 
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8

An experimental investigation of the flap-lag-torsion aeroe..:

Sharpe, David L ; United States. Army Aviation Research and Technology Activity. Aeroflightdynamics Directorate ; Ames Research Center
http://hdl.handle.net/2027/uiug.30112106614198.  , 1986
Link: http://hdl.handle.net/20..
 
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9

Predicted effect of dynamic load on pitting fatigue life fo..:

Lewicki, David G. org. AVSCOM ; United States. Army Aviation Systems Command ; United States. Army Aviation Research and Technology Activity. Propulsion Directorate..
http://hdl.handle.net/2027/uiug.30112106613604.  , 1986
Link: http://hdl.handle.net/20..
 
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10

Aerodynamic characteristics of several current helicopter t..:

Wilson, John C. org. AVSCOM ; Kelley, Henry L. org. AVSCOM ; United States. Army Aviation Research and Technology Activity. Aerostructures Directorate...
http://hdl.handle.net/2027/uiug.30112106614446.  , 1986
Link: http://hdl.handle.net/20..
 
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11

Effects of planform geometry on hover performance of a 2-me..:

Phelps, Arthur E. org AVSCOM ; Althoff, Susan L. org AVSCOM ; Langley Research Center...
http://hdl.handle.net/2027/uiug.30112106616631.  , 1986
Link: http://hdl.handle.net/20..
 
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12

Portfolio optimization by means of multiple tandem certaint..:

Chow, Brian G , 2013
Link: https://www.jstor.org/st..
 
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13

National water resources challenges facing the U.S. Army Co..:

, 2011
Link: https://search.ebscohost..
 
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14

Advances in low-carbon high strength ferrous alloys: LCFA-9 

Key engineering materials, v. 84-85
Mohanty, O. N ; Rath, B. B ; Imam, M. A. , 1993
Link: https://search.ebscohost..
 
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