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Showing 10 out of a total of 367 results for collection: Aeronautical Research Council Reports & Memoranda.
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Pressure measurements on a slender rhombic cone at incidence at Mach numbers from 0.4 to 1.1
J. H. B. Smith
;
A. G. Kurn
(
1968
)
Some exact calculations of the lift and drag produced by a wedge in supersonic flow, either directly or by interference
P. L. Roe
(
1964
)
Wind Tunnel Tests on a Streamlined Fan-Lift Nacelle Part I. Tests on Nacelle Alone and with Wings or Underfins Fitted Part II. The effect of Forward Speed on the Lift Produced by a Lifting Fan and its Inlet
J. E. Hackett
(
1965
)
Experiments on two-dimensional base flow at subsonic and transonic speeds
J. F. Nash
;
V. G. Quincey
;
J. Callinan
(
1963
)
An experimental investigation of wall-interference effects on dynamic measurements on half-models in ventilated tunnels through the transonic speed range
A. W. Moore
;
K. C. Wight
(
1967
)
Wind tunnel studies of leading edge separation phenomena on a quarter-scale model of the outer panel of the handley page "Victor" wing, with and without nose droop
R. A. Wallis
(
1965
)
An analysis of two-dimensional turbulent base flow, including the effect of the approaching boundary layer
J. F. Nash
(
1962
)
Flutter characteristics of a wing carrying a flexibly mounted mass
D. R. Gaukroger
(
1961
)
A note on the theory of parachute stability
W. G. S. Lester
(
1962
)
An investigation of the flow about circular cylinders placed normal to a low-density, supersonic stream
S. C. Metcalf
;
C. J. Berry
;
B. M. Davis
(
1964
)
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E. W. E. Rogers (9)
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