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)

On the driver-reservoir technique.
by: Davies, L.
Published: (1968)

Measurement of the internal performance of a rectangular air-intake at Mach number of 0.9 /
by: Brown, C. S. (Aerospace engineer), et al.
Published: (1976)

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

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

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)

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)

Notes on the automatic control of a blowdown wind tunnel /
by: Pugh, P. G., et al.
Published: (1969)

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

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

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

Measurement of turbulence in the Liverpool University turbomachinery wind tunnels and compressor /
by: Shaw, R. (Ronald), 1924-, et al.
Published: (1966)

Measurement of the internal performance of a rectangular air intake with variable geometry at Mach numbers from 1.7 to 2.5.
by: Brown, C. S. (Charles Scorer), et al.
Published: (1973)

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)

A control-surface oscillatory derivative rig for use with half-models in high-speed wind tunnels /
by: Wight, K. C., et al.
Published: (1976)

Free-flight measurements of the incremental drag due to engine nacelles on a transonic swept-wing aircraft / by G.K. Hunt.
by: Hunt, G. K.
Published: (1967)

Low-speed wind-tunnel tests of a two-dimensional wing fitted with two plain differentially-deflected trailing-edge flaps /
by: McKie, John (Aerodynamicist)
Published: (1975)

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)

An application of fast frequency-sweep excitation to the measurement of sub-critical response of a low speed wind tunnel model /
by: Skingle, C. W. (Colin William)
Published: (1976)

Wind tunnel flutter tests at subsonic speeds on a half-wing with a fan engine nacelle /
by: Drane, D. A., et al.
Published: (1976)

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 wind-tunnel investigation of the roll stability of a 1/5 scale model of the short SC 1 at large sideslip /
by: Trebble, W. J. G.
Published: (1968)

Measurement of the internal performance of a rectangular air intake having variable geometry compression surfaces at Mach numbers from 1.7 to 2.5.
by: Brown, C. S. (Charles Scorer), et al.
Published: (1973)

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)