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Aeronautical Research Council: Recent submissions
Now showing items 1621-1640 of 2786
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Fortran subroutines for finite element analysis
B. C. Merrifield
(
1972
)
Optimum engine thrust deflection for high-speed cruising aircraft
J. Pike
(
1972
)
Some experiences with "on-line" spectral analysis using a small digital computer
J. B. Roberts
;
D. Surry
;
R. F. Johnson
(
1972
)
Dynamic calibration of gas flowmeters
K. R. Maslen
(
1972
)
A result concerning the supersonic flow below a plane delta wing
P. L. Roe
(
1972
)
Transonic fan noise
D. Hawkings
(
1972
)
An examination of an iterative procedure for determining the characteristic exponents of linear differential equations with periodic coefficients
D. L. Woodcock
;
D. Elton
;
R. J. Davies
(
1972
)
The design of high sensitivity pressure transducers for use in shock-tunnels
R. O. Goodchild
;
L. Bernstein
(
1972
)
The effect of an application of heat on the fatigue performance under random loading of a notched specimen of DTD 5014 (RR58) material
J. R. Heath-Smith
;
Judy E. Aplin
(
1972
)
Andover C. Mk. 1 airfield criteria trials
J. Howell
(
1972
)
A laboratory comparison of three methods of personal conditioning
J.R. Allan et al
(
1972
)
Some modifications to the calculation method for wings with part-span extending-chord flaps given in rae technical report 69034
J. McKie
(
1972
)
Heat transfer and surface pressure measurements on two conical wings in free flight up to M
G. H. Greenwood
(
1972
)
Fortran Programmes for Axisymmetric Potential Flow Around Closed and Semi-Infinite Bodies
C. M. Albone
(
1972
)
Two programmes are presented in I.C.L. FORTRAN, for the pressure distribution on the surface of an arbitary body of revolution in axisymmetric, incompressible flow. One programme evaluates the pressure distribution on an ...
A computer program to calculate the pressure distribution on an annular aerofoil
C. Young
(
1972
)
An investigation of transition fixing technique for a 10.5% thick, 28 degrees sweptback wing at high subsonic speeds and R is semilar to 3 x 106
P. G. Hutton
(
1972
)
A comparison of the surface-source solution with an exact solution for the twodimensional inviscid flow about a slotted-flap aerofoil
B. R. Williams
(
1972
)
Notes on the internal drag, lift and pitching moment of a ducted body
J. W. Britton
;
M. D. Dobson
(
1972
)
Spontaneous ignition of avtur vapour in various oxygen-nitrogen mixtures
J. T. Cansdale
(
1972
)
Some measurements of base pressure fluctuations at subsonic and supersonic speeds
D. G. Mabey
(
1972
)
Now showing items 1621-1640 of 2786
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