Potential benefits of magnetic suspension and balance systems /

Wind-tunnel investigation of a full-scale canard-configured general aviation airplane /
by: Yip, Long P.
Published: (1985)

Validation of 3-D ice accretion measurement methodology for experimental aerodynamic simulation /
by: Broeren, Andy P.
Published: (2015)

Unsteady aerodynamic model tuning for precise flutter prediction /
by: Pak, Chan-gi, 1956-
Published: (2011)

Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-by 6-foot supersonic wind tunnel /
by: Castner, Raymond S., et al.
Published: (2018)

Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets /
by: Kelley, Henry L.
Published: (1990)

Theory of wing rock /
by: Hsu, Chung-Hao
Published: (1984)

Prediction of vortex-induced loads on wind tunnel turning vanes /
by: Ross, James C., 1965-
Published: (1985)

FORTRAN programs for calculating wind-tunnel boundary interference /
by: Heyson, Harry H.
Published: (1969)

Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivatives for the X-29A aircraft /
by: Budd, Gerald D.
Published: (1984)

Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes /
by: Sutliff, Daniel L. (Daniel Linden), 1962-, et al.
Published: (2014)

Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode /
by: Lance, Michael B.
Published: (1991)

Further investigation into calibration techniques for a magnetic suspension and balance system /
by: Eskins, J.
Published: (1986)

FLEXWAL : a computer program for predicting the wall modifications for two-dimensional solid, adaptive-wall wind tunnels /
by: Everhart, Joel L.
Published: (1983)

Application of approximate unsteady aerodynamics for flutter analysis /
by: Pak, Chan-gi
Published: (2010)

Tabulation of data from tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
by: Jenkins, Renaldo V.
Published: (1983)

Modern airfoil ice accretions /
by: Addy, Harold E., Jr., 1960-, et al.
Published: (1997)

Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft /
by: Klein, Vladislav
Published: (1997)

Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade /
by: Noonan, Kevin W.
Published: (1990)

Sensitivity analysis for coupled aero-structural systems /
by: Giunta, Anthony A.
Published: (1999)

Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses /
by: Harris, Charles D., 1952-
Published: (1972)

Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover /
by: Watkins, Anthony Neal
Published: (2018)

Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation /
by: Lin, Jensen, et al.
Published: (2000)

Analysis of a split-plot experimental design applied to a low-speed wind tunnel investigation /
by: Erickson, Gary E.
Published: (2013)

Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /
by: Mack, Robert J.
Published: (1999)

Subsonic dynamics of stardust sample return capsule /
by: Mitcheltree, Robert A. (Robert Alan), 1961-, et al.
Published: (1997)

Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall /
by: Everhart, Joel L.
Published: (1994)

Development of experimental icing simulation capability for full-scale swept wings : hybrid design process, years 1 and 2 /
by: Fujiwara, Gustavo
Published: (2017)

Aero-thermal calibration of the NASA Glenn Icing Research Tunnel (2012 tests) /
by: Christine Pastor-Barsi, et al.
Published: (2013)

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /
by: Penland, Jim A., et al.
Published: (1979)

Flow-visualization techniques used at high speed by configuration aerodynamics wind-tunnel-test team /
Published: (2001)

Wind-tunnel investigations of blunt-body drag reduction using forebody surface roughness /
by: Whitmore, Stephen A., et al.
Published: (2001)

Exploratory low-speed wind-tunnel study of concepts designed to improve aircraft stability and control at high angles of attack /
by: Hahne, David E. (David Edgar)
Published: (1985)

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel /
by: Schairer, Edward T.
Published: (1989)

Study of the integration of wind tunnel and computational methods for aerodynamic configurations /
by: Browne, Lindsay E.
Published: (1989)

Design of a slotted, natural-laminar-flow airfoil for a transport aircraft /
by: Somers, Dan M.
Published: (2019)

Wind-tunnel investigation of a full-scale canard-configured general aviation airplane /
by: Yip, Long P.
Published: (1985)