Some exploratory tests on a two-dimensional blowncylinder model in R.A.E. 2 ft. x 1 1/2 ft. transonic-wind tunnel /

Transonic wind tunnel testing /
by: Goethert, B. H.
Published: (1961)

Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System /
Published: (2001)

The motion of helicopter blades at low rotor speeds in high winds /
by: Willmer, M. A. P.
Published: (1966)

The flapping behaviour of a helicopter rotor at high tip-speed ratios /
by: Wilde, Ernest
Published: (1966)

Experimental pressure distributions on a plane-nosed cylinder at subsonic and transonic speeds /
by: Stanbrook, A.
Published: (1966)

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)

Development of a large field of view shadowgraph system for a 16 ft. transonic wind tunnel /
by: Talley, Michael A.
Published: (2000)

Transonic aerodynamic testing : January 17-21, 1972.
Published: (1972)

Transonic aerodynamics : technical papers selected from the Transonic Perspective Symposium, Moffett Field, California, February 18-20, 1981 /
Published: (1982)

Transonic wind tunnel test of a 14% thick oblique wing /
Published: (1990)

Unsteady transonic aerodynamics /
Published: (1989)

Towards new transonic windtunnels /
Published: (1979)

Calculation of three-dimensional unsteady transonic flows past helicopter blades /
by: Chattot, J. J.
Published: (1980)

Analytical models for rotor test module, strut, and balance frame dynamics in the 40- by 80-ft wind tunnel /
by: Johnson, Wayne, 1946-
Published: (1976)

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

Some anomalies observed in wind-tunnel tests of a blunt body at transonic and supersonic speeds /
by: Brooks, Joseph D.
Published: (1976)

Control of the NASA Langley 16-foot transonic tunnel with the self-organizing feature map /
by: Motter, Mark A.
Published: (1998)

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

The R.A.E. 4-ft x 3-ft experimental low-turbulence wind tunnel. : Part IV. Further turbulence measurements /
by: Schuh, H. (Herbert)
Published: (1962)

The NASA Langley 16-foot transonic tunnel : historical overview, facility description, calibration, flow characteristics, and test capabilities /
Published: (1995)

An experimental investigation of wall-interference effects on dynamic measurements on half-models in ventilated tunnels through the transonic speed range /
by: Moore, A. W. (Alan William)
Published: (1969)

Free-flight tests of vortex generator configurations at transonic speeds /
by: Edwards, J. B. W.
Published: (1966)

Two-dimensional wind tunnel.
Published: (1982)

The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds /
by: Wilby, P. G.
Published: (1967)

Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip /
by: Yeager, William T.
Published: (1997)

Results of the integration of a transonic full-potential analysis program with a free-wake lifting-line program for hovering rotors /
by: Chung, Song-Young
Published: (1987)

The reduction of dynamic interference by sound-absorbing walls in the RAE 3ft wind tunnel /
by: Mabey, Dennis G.
Published: (1979)

Modeling and control study of the NASA 0.3-meter transonic cryogenic tunnel for use with sulfur hexafluoride medium /
by: Balakrishna, S.
Published: (1992)

Measurements of control-surface oscillatory derivatives on a sweptback, tapered model wing in two transonic tunnels /
by: Lambourne, N. C.
Published: (1977)

The pressure distribution at zero lift on a slender delta wing at transonic speeds /
by: Firmin, Michael Charles Peter, 1929-
Published: (1968)

Wind-tunnel/flight correlation, 1981 : proceedings of a miniworkshop held at NASA Langley Research Center, Hampton, Virginia, November 19-20, 1981 /
Published: (1981)

Wind-tunnel acoustic results of two rotor models with several tip designs /
by: Martin, R. M. (Ruth McVoy), 1956-
Published: (1986)

The new system for controlling the attitude and motivator deflections of a model in the R.A.E. No. 19 wind tunnel /
by: Pecover, B. E.
Published: (1968)

Three-dimensional flow field measurements in a transonic turbine cascade /
by: Giel, P. W.
Published: (1996)

Wind tunnel tests of rotor blade sections with replications of ice formations accreted in hover /
by: Lee, John D.
Published: (1986)

Wind tunnel test of 0.2 scale model of Bell helicopter M222 : test number 8009 /
by: Nicks, Oran W.
Published: (1980)