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AERADE: Recent submissions
Now showing items 2581-2600 of 3498
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Cabin conditioning tests on a simulated M 2.2 transport aircraft cabin
T. L. Hughes
;
E. A. Timby
(
1968
)
Solution of the catapult take-off performance equations by an analogue method
E. W. Addicott
;
R. W. Jones
(
1968
)
Experiments on methods for the numerical solution of a certain non-linear biharmonic equation
M. R. Abbott
(
1968
)
Optimum fibre arrangements for reinforced sheets under combined loading
G. Z. Harris
(
1968
)
Civil aircraft airworthiness data recording programme study of severe turbulence encountered by civil aircraft
G. E. King
(
1967
)
Leading edge effects on caret wings
J. C. Cooke
(
1968
)
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
)
Now showing items 2581-2600 of 3498
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