Tests at a mach number of 2.0 on a rectangular twin-duct air intake with variable geometry : situated in the flow field of a slender wing /

Tests at M= 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing /
by: Griffiths, R. T.
Published: (1969)

An analogue computer for on-line correction of wind-tunnel force and moment data /
by: Pecover, B. E.
Published: (1967)

Determination of stagnation temperatures in the R.A.R.D.E. hypersonic gun tunnel from streak camera measurements of flow velocity /
by: Bowman, J. E.
Published: (1967)

A technique for the wind tunnel simulation of store release at high speeds /
by: Beecham, L. J.
Published: (1966)

The response times of typical transducer-tube configurations for the measurement of pressures in high-speed wind tunnels /
by: Larcombe, M. J.
Published: (1966)

Characteristics of high-speed wind tunnels in the United Kingdom relevant to aeroelastic-model tests /
by: Irwin, C. A. K.
Published: (1967)

Wall corrections to longitudinal components measured on wind-tunnel models with tails /
by: Lovell, D. A.
Published: (1969)

A method for correcting measurements of the heat transfer factor through the skin of a wind tunnel model /
by: Piggott, Brian Alexander Martin
Published: (1966)

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)

A study on the running times in reflected shock tunnels /
by: Ackroyd, J. A. D.
Published: (1967)

A short time response stagnation temperature probe /
by: East, R. A.
Published: (1967)

Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel /
by: Bowman, J. E.
Published: (1967)

The accuracy of pressure transducers when used in short-duration wind-tunnel facilities /
by: Pennelegion, L.
Published: (1967)

An ejector-driven wind tunnel for the generation of turbulent flows with arbitrary mean velocity profile /
by: Teunissen, H. W.
Published: (1969)

Low-speed wind-tunnel tests of a number of fin configurations on a flat-plate gothic wing of unit aspect ratio /
by: Peckham, D. H.
Published: (1969)

A control and measurement system for aeroelastic model tests /
by: Hicks, William Desmond Thomas
Published: (1969)

Measurements of secondary flow in the boundary layers of a 180 degree channel /
by: Patel, V. C. (Virendrakumar Chaturbhai)
Published: (1969)

Super VC 10 cruise drag-A wind-tunnel investigation /
by: Taylor, C. R.
Published: (1970)

Bulk compressibility effects in the R.A.R.D.E. no. 3 hypersonic gun tunnel /
by: Clayden, W. A.
Published: (1966)

Some exploratory tests on a two-dimensional blowncylinder model in R.A.E. 2 ft. x 1 1/2 ft. transonic-wind tunnel /
by: Jones, A. F.
Published: (1967)

Subsonic tests in free molecule flow on impact tube pressure probes having a wide range of tube lengths at angles of attack up to 90 ̊ /
by: Hughes, Peter C. (Peter Carlisle), 1940-
Published: (1965)

Finite difference solutions for an unsteady interference parameter in slotted wind tunnels /
by: Rushton, K. R.
Published: (1969)

Interference effects at M=8.5 of wires and probes on the wake of a magnetically suspended rounded base cone /
by: Crane, John Frank William
Published: (1970)

Low-speed tunnel tests of an aspect-ratio 9 jet-flap model, with ground simulation by moving-belt rig /
by: Butler, S. F. J.
Published: (1966)

Note on the evaluation of solid-blockage corrections for rectangular wind tunnels with slotted walls /
by: Acum, Wilfred Ethelbert Aldred
Published: (1962)

Wall corrections for wings oscillating in wind tunnels of closed rectangular section /
by: Acum, Wilfred Ethelbert Aldred
Published: (1963)

Cavity heating experiments supporting Shuttle Columbia accident investigation /
Published: (2011)

Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds /
by: Rossiter, J. E.
Published: (1967)

The change in shock-tunnel tailoring Mach number due to driver gas mixtures of helium and nitrogen /
by: Pennelegion, L.
Published: (1965)

Advanced hypersonic test facilities /
Published: (2002)

Experiments with cones in low-density flows at Mach numbers near 2 /
by: Rogers, E. W. E.
Published: (1967)

Mach number measurements in high-speed wind tunnels /
by: Hill, Jacques A. F.
Published: (1956)

Wind-tunnel experiments on a rectangular-wing jet-flap model of aspect-ratio 6 /
by: Alexander, A. J.
Published: (1964)

Upwash interference in a rectangular wind tunnel with closed side walls and porous slotted floor and roof /
by: Holder, D. R.
Published: (1963)

The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)

NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /
by: Wolf, Stephen W. D., et al.
Published: (1997)