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Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard regio

Noonan, Kevin W.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

Airloads, wakes, and aeroelasticity

Johnson, Wayne.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1990] 1990

Design of an active helicopter control experiment at the Princeton Rotorcraft Dynamics Laboratory in

Marraffa, Andrew M.
[Moffett Field, Calif.] : NASA Ames Research Center, [1989] 1989

Design of helicopter rotor blades for optimum dynamic characteristics

[St. Louis, MO. : Dept. of Mechanical Engineering, Washington University, [Hampton, Va. : Langley Research Center, 1982-1985] 1985

Development of ROT22 DATAMAP interface

Shenoy, K. R.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1986] 1986

Documentation of ice shapes accreted on the main rotor of a UH-1H Helicopter in level flight final r

Hanson, M. K.
Columbus, Ohio : Ohio State University, Aeronautical and Astronautical Research Laboratory ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1986] 1986

The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability

Bousman, William G.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

Experimental study of main rotor tip geometry and tail rotor interactions in hover

Balch, D. T.
Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, [1985] 1985

Loads and performance data from a wind-tunnel test of generic model helicopter rotor blades

Yeager, William T.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2005] 2005

A new methodology for free wake analysis using curved vortex elements

Bliss, Donald B.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987. 1987

A novel potential viscous flow coupling technique for computing helicopter flow fields

Summa, J. Michael.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1990] 1990

Simple theoretical models for composite rotor blades

Valisetty, Ramakrishna Rao, 1949- author.
Atlanta, Georgia : Georgia Institute of Technology. School of Aerospace Engineering ; [Washington, DC] : National Aeronautics and Space Administration, 1984. 1984

Study for prediction of rotor/wake/fuselage interference

Clark, D. R.
Redmond, WA : Analytical Methods, Inc. ; Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, [1985] 1985

Unsteady aero computation of a 1 1/2 stage large scale rotating turbine

To, Wai-Ming.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012