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Aeronautical Research Council Current Papers: Recent submissions
Now showing items 641-660 of 1393
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Measurements of skin-friction in an annulus by the floating element technique
J. K. White
;
R. E. Franklin
(
1965
)
Influence of chemical contouring on the fatigue and sustained load properties of high tensile steel sheet
Westland Aircraft Limited
;
Saunders-Roe Division
(
1965
)
Theoretical investigation of some basic assumptions of Schlichting's singularity method of cascade analysis
R. I. Lewis
;
G. A. Pennington
(
1965
)
The unsteady motion of slender wings with leading-edge vortices
B. D. Dore
(
1965
)
The chemical contouring of 3 percent chromium-molybdenum-vanadium and 5 percent chromium-molybdenum-vanadium high strength steel sheet
Bristol Aerojet Ltd
(
1965
)
Potential flow through cascades extensions to an exact theory
J. P. Gostelow
(
1965
)
Potential flow through cascades a comparison between exact and approximate solutions
J. P. Gostelow
(
1965
)
On the calculation of cascade flows
W. S. Hall
;
B. Thwaites
(
1965
)
Tests with a variable ramp intake having combined external/internal compression, and a design mach number of 2.2
M. C. Neale
;
P. S. Lamb
(
1965
)
Wind tunnel measurements of the far-field pressures due to some lifting, slender delta wings
T. A. Cook
(
1965
)
An experimental investigation into the determination of lift from wake traverses at supersonic speeds
J. Wooller
;
M.C.P. Firmin
(
1965
)
List of current papers (numbers 751-800)
Aeronautical Research Council
(
1965
)
Wind tunnel tests at mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on a slender, cambered ogee wing
T. A. Cook
(
1965
)
Wind tunnel measurements at mach numbers up to 2.80 of the effects of gulling on the longitudinal and lateral stability and drag of a cambered, slender ogee wing
T. A. Cook
(
1965
)
The steady flow of a viscous fluid past a circular cylinder
S. C. R. Dennis
;
M. Shimshoni
(
1965
)
Wind tunnel tests at mach numbers up to 1.8 on a model with .03 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188)
E.P. Sutton
;
P.G. Hutton
;
L.C. Squire
(
1965
)
The design and development of an air-bearing for the measurement of damping in yaw on a jet-blowing model
A. P. Cox
(
1965
)
The calculation of aircraft motion in design rolling manoeuvres
D. J. Eckford
(
1965
)
Pressure distribution measurements on a series of slender delta body shapes at mach numbers of 6.85 and 8.60
D. H. Peckham
(
1965
)
A comparison of rivet shear strengths obtained from two-rivet specimens and from multi-rivet specimens at room temperature and 150 degrees C
D. F. Wright
;
P. Judson
;
P. W. Horrocks
(
1965
)
Now showing items 641-660 of 1393
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