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Aeronautical Research Council Current Papers: Recent submissions
Now showing items 481-500 of 1393
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The drag of some wedge centre-body intakes at mach numbers of 1.56, 1.86 and 2.14
R. A. Dutton
;
E. L. Goldsmith
(
1967
)
An investigation into a technique for measuring jet interference effects using free-flight models
G. H. Greenwood
(
1967
)
Potential flow theory for tandem cascade by Howell's method
Y. M. Yip
;
J. W. Railly
(
1967
)
Guided weapons aerodynamic study force and moment measurements on some monoplane and cruciform slender wing-body combinations at M 4. 0
P. L. Roe
(
1968
)
The distribution of a wall pressure rise in a turbulent boundary layer
R.J. Herd
(
1967
)
A survey of the thermal conductance of metallic contacts
H. Y. Wong
(
1968
)
Techniques for tests on structures subject to kinetic heating
P. Talbot
(
1967
)
Heat transfer in the vicinity of a 15 degrees compression corner at mach numbers from 2.5 to 4.4
R. C. Hastings
;
C. S. Brown
;
Susan Atkinson
(
1967
)
The calculation of momentum thickness in a turbulent boundary layer at mach numbers up to unity
J. F. Nash
;
A. G. J. Macdonald
(
1967
)
Some further notes on the laminar boundary layer development and running time in a shock tube
J. A. D. Ackroyd
(
1967
)
A preliminary experimental investigation of shock-wave development on aerofoils
T. H. Moulden
;
I. J. Cox
;
V. A. Stringfellow
(
1967
)
The effect of base bleed on the base pressure of several shrouded and unshrouded propelling nozzles at M
M.M. Shaw
(
1967
)
The influence of gas streams and magnetic fields on electric discharges part 3 arcs in transverse magnetic fields at atmospheric pressure
V. W. Adams
(
1967
)
The velocity field near non-lifting delta wings according to supersonic linearized theory
R. S. Bartlett
(
1967
)
Computer programmes to calculate the response of flexible aircraft to gusts and control movements
C. G. B. Mitchell
(
1967
)
Free-flight measurements of the incremental drag due to engine nacelles on a transonic swept-wing aircraft
G. K. Hunt
(
1967
)
Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5 degrees semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8
G. H. Greenwood
(
1967
)
Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel
J. E. Bowman
(
1967
)
List of current papers (numbers 901-950)
Aeronautical Research Council
(
1967
)
Measurements of wing buffeting on a scimitar model
D. G. Mabey
(
1967
)
Now showing items 481-500 of 1393
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