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Showing 10 out of a total of 56 results for collection: Aeronautical Research Council Reports & Memoranda.
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Vectorial analysis of flight flutter test results
E. G. Broadbent
;
E. Violet Hartley
(
1958
)
10-ft x 7-ft tunnel tests up to M = 0.94 of nose droop and a blunt-nosed NACA 3-00 type section on a 7.5 per cent thick 50 deg swept wing
A. L. Courtney
(
1958
)
The centre-line mach-number distributions and auxiliary-suction requirements for the A.R.A. 9-ft X 8-ft transonic wind tunnel
A. B. Haines
;
J. C. M. Jones
(
1958
)
Seaplane impact a review of theoretical and experimental results
T. Arlotte et al
(
1958
)
The calculation of lift slopes, allowing for boundary layer, with applications to the RAE 101 and 104 aerofoils
D. A. Spence
;
J. A. Beasley
(
1958
)
Simplified loading formulae for pull-out manoeuvres of tailed aeroplanes
S. Neumark
(
1958
)
The theoretical evaluation of the downwash behind jet-flapped wings
A. J. Ross
(
1958
)
Notes on the progress of free-flight trials to measure heat transfer at Mach numbers up to 5
J. Picken
;
R. Harmer
(
1958
)
Flexible Mass-Balance Arms and Control-Surface Flutter
D. Moxon
(
1958
)
Heat-transfer and skin-friction measurements at a mach number of 2.44 for a turbulent boundary layer on a flat surface and in regions of separated flow
G. E. Gadd
;
W. F. Cope
;
J. L. Attridge
(
1958
)
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Author
A. J. Ross (2)
G. E. Gadd (2)
J. H. Foxwell (2)
J. P. Jones (2)
N. Curle (2)
R. E. Franklin (2)
R. Staniforth (2)
A. B. Haines (1)
A. D. N. Smith (1)
A. D. S. Carter (1)
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Date Issued
1958 (56)