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Showing 10 out of a total of 636 results for collection: Aeronautical Research Council Current Papers.
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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 measurement of sub-critical damping on the R.A.E. flutter simulator
J. Appleton
;
W. D. Hicks
(
1961
)
Exploratory tests on sting interference at a mach number of 6.8
D. H. Peckham
(
1961
)
CANCELLED AS CP
Unknown author
(
1961
)
Wind tunnel tests at Mach numbers between 0.6 and 1.4 of a 60 degrees swept wing having an aerofoil section designed for subcritical flow at a Mach number of 1.2 part 1 9 percent thick section with "triangular" pressure distribution
E. F. Lawlor
(
1962
)
An experimental investigation of the two-dimensional wall jet
James H. Whitelaw
(
1967
)
The 7 in. x 7 in. hypersonic wind tunnel at R.A.E. Farnborough part 4 measurements of diffuser performance, blockage, starting loads and humidity
J. F. W. Crane
;
J. G. Woodley
(
1963
)
Pressure measurements on a cone-cylinder-flare configuration at small incidences for M
J. G. Woodley
(
1963
)
The development of a static tube which is insensitive to incidence at supersonic speeds
J. E. G. Townsend
(
1961
)
Scale models for thermo-aeroelastic research
W. G. Molyneux
(
1961
)
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Aeronautical Research Council (17)
D. H. Peckham (8)
J. C. Cooke (8)
G. T. Golesworthy (7)
L. Davies (7)
M. C. Neale (7)
D. G. Mabey (6)
G. K. Hunt (6)
J. F. Nash (6)
N. I. Bullen (6)
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1965 (80)
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