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Aeronautical Research Council: Recent submissions
Now showing items 2121-2140 of 2786
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Prandtl-Meyer flow in a relaxing gas
P. A. Blythe
(
1964
)
On the theory of vibrational relaxation in gases
E. Wild
(
1964
)
Some studies of pressure distributions on the windward surfaces of conical bodies at high supersonic speeds
A. Akers
(
1966
)
Calculation of the turbulent boundary layer in the nozzle of an intermittent axisymmetric hypersonic wind tunnel
N. B. Wood
(
1964
)
Measurements of the free stream turbulence in the R.A.E. bedford 13 ft x 9 ft wind tunnel
D. H. Ferriss
(
1964
)
A study on the running times in shock tubes
J. A. D. Ackroyd
(
1964
)
Calculations of the structure of unsteady rarefaction waves in oxygen/argon mixtures, allowing for vibrational relaxation
J. P. Appleton
(
1966
)
Pressure, heat transfer and temperature measurements in the two-dimensional nozzle of a reflected-shock tunnel
J. L. Stollery
;
J. E. G. Townsend
(
1964
)
Atmospheric turbulence encountered by comet 2 aircraft carrying cloud collision warning radar
Judy E. Aplin
(
1964
)
A correlation of the forebody drag of cylinders with plane and hemispherical noses at mach numbers from zero to 2.5
A. Stanbrook
(
1964
)
Discrepancies between theoretical and experimental values of temperature behind a shock wave
J. Wilson
(
1964
)
Wind-tunnel experiments on a simple lifting-jet body with and without wings
W. J. G. Trebble
(
1964
)
Measurements of skin-effection using surface-pitot tubes in free flight at supersonic speeds
J. B. W. Edwards
(
1964
)
Measurements of "aquaplaning height" on a meteor aircraft, and photos of flow pattern under a model tyre
W. E. Gray
(
1964
)
Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177), with blowing over the trailing-edge flaps and ailerons
S. F. J. Butler
;
M. B. Guyett
(
1966
)
Some tests with trapped vortices in supersonic flow
B. S. Stratford
;
M. C. Neale
(
1964
)
A comparison of the measured and predicted flutter characteristics of a wing-aileron-tab model
H. Hall
(
1965
)
Flutter tests and calculations on an all-moving model fin
J. K. Curran
(
1964
)
The calculation of pressure distribution in steady supersonic flow, with arbitrary downwash distribution
Laura Klanfer
(
1965
)
A note on the estimation of the effect of wind tunnel walls on the forces on slowly oscillating slender wings
W. E. A. Acum
(
1965
)
Now showing items 2121-2140 of 2786
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