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Aeronautical Research Council: Recent submissions
Now showing items 2001-2020 of 2786
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The motion of helicopter blades at low rotor speeds in high winds
M. A. P. Willmer
(
1966
)
The role of compressive stress in the load and strain fatigue behaviour of H.46 at room temperature
G. P. Tilly
(
1966
)
Vertical accelerations due to structural vibrations of a slender aircraft flying in continuous turbulence
J. K. Zbrozek
(
1966
)
The magnetic deflection of short arcs rotating between annular electrodes above and below atmospheric pressure
E. D. Blix
;
A. E. Guile
(
1966
)
The lateral oscillation of slender aircraft
A. J. Ross
(
1966
)
The performance of a centrebody propelling nozzle with a parallel shroud in external flow part 1
R. J. Herd
;
G. T. Golesworthy
(
1966
)
The chance of a rough flight
N. I. Bullen
(
1965
)
Interim report on low-speed flight tests of a slender-wing research aircraft (Handley-page H.P.115)
P. L. Bisgood
;
C. O. O'Leary
(
1966
)
Handling qualities of aircraft with marginal longitudinal stability
T.B. Saunders
(
1966
)
Comparison of seven wing buffet boundaries measured in wind tunnels and in flight
D. G. Mabey
(
1966
)
The interpretation of strain measurements for flight load determination
P. B. Hovell
;
D. A. Webber
;
T. A. Roberts
(
1966
)
An experimental check on the theoretical relationship between the spectral density and the probability distribution of crossings for a stationary random process with Gaussian distribution, using data obtained in measurements of aircraft response to turbul
J. Burnham
(
1965
)
Preston tube measurements in turbulent boundary layers and fully developed pipe flow
D. H. Ferriss
(
1965
)
Review of general operating experience with a jet-lift VTOL research aircraft (short S.C.1)
D. Lean
;
H. W. Chinn
(
1965
)
A survey of aircraft handling criteria
C. Leyman
;
E. R. Nuttall
(
1966
)
Turbulent-boundary-layer behaviour and the auxiliary equation
John F. Nash
(
1966
)
A unified theory of friction, heat transfer and mass transfer in the turbulent boundary layer and wall jet
D. B. Spalding
(
1965
)
Slender-body theory calculations of the effect on lift and moment of mounting the wing off the fuselage centre-line
R. S. Bartlett
(
1965
)
Further tests with a variable ramp intake having a design mach number of 2.2
M. C. Neale
;
P. S. Lamb
(
1966
)
The time required for high speed airstreams to disintegrate water drops
D. C. Jenkins
;
J. D. Booker
(
1965
)
Now showing items 2001-2020 of 2786
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