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Acoustically tailored composite rotorcraft fuselage panels

Hambric, Stephen A., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2015. 2015-

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

Aircraft design considerations to meet one engine inoperative (OEI) safety requirements

Scott, Mark W., author.
Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 2012. 2012

Assessment of High Temperature Superconducting (HTS) electric motors for rotorcraft propulsion

Doernbach, Jay.
[Washington, D.C.] : National Aeronautics and Space Administration, [1990] 1990

Assessment of NASA's aircraft noise prediction capability

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

Development and validation of a multidisciplinary tool for accurate and efficient rotorcraft noise p

Liu, Yi.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Development of rotorcraft interior noise control concepts phase II, full scale testing

Yoerkie, C. A.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986] 1986

Extension of a three-dimensional viscous wing flow analysis

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Far-field acoustic power level and performance analyses of F31/A31 open rotor model at simulated sca

Sree, Dave, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2015. 2015-

Investigation of active flow control to improve aerodynamic performance of oscillating wings

Narducci, Robert P., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2014. 2014-

NDARC NASA Design and Analysis of Rotorcraft

Johnson, Wayne, 1946-
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [2009] 2009

RotCFD analysis of the AH-56 Cheyenne hub drag

Solis, Eduardo, author.
Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, October 2016. 2016-

Rotorcraft application of advanced computational aerodynamics

Stanaway, Sharon K.
San Jose, Calif. : MCAT Institute ; [Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, Va. : For sale by the National Technical Information Service, 1991] 1991

Rotorcraft transmission noise path model, including distributed fluid film bearing impedance modelin

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft

Parrish, Russell V.
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

Technology assessment for large vertical-lift transport tiltrotors

Germanowski, Peter J.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [2010] 2010

Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-sy

Wilbur, Matthew L., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 1998. 1998-