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AERADE: Recent submissions
Now showing items 3361-3380 of 3498
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A criterion for the prediction of the recovery characteristics of spinning aircraft
T. H. Kerr
(
1955
)
A note on the sound from weak disturbances of a normal shock wave
Alan Powell
(
1955
)
Tests on a swept-back wing and body with endplates and wing tip tanks in the compressed air tunnel
C. Salter
;
R. Jones
(
1954
)
Wide range amplifier for turbulence measurements with adjustable upper frequency limit
H. Schuh
;
D. Walker
(
1955
)
Some visual observations of the flow over a swept-back wing in a water tunnel, with particular reference to high incidences
M. C. Lambourne
;
P. S. Pusey
(
1955
)
Report of the definitions panel on the definitions of the thrust of a jet engine and of the Internal Drag of a ducted body
Aeronautical Research Council
(
1955
)
The use of quartz in the manufacture of small diameter pitot tubes
J.R. Cooke
(
1955
)
Measurement of lift, pitching moment and hinge moment on a two-dimensional RAE 102 aerofoil
A. S. Batson
(
1953
)
Shadowgraphs of model projectiles fired at high mach numbers and near M = 1 in the N.P.L. Ballistic range
W. F. Cope
(
1955
)
Note on the flow near the tail of a two-dimensional aerofoil moving at a free-stream mach number close to unity
D. W. Holder
(
1955
)
Load diffusion in plastic structures
L.M. Tucker
;
R.B. Twiss
(
1955
)
Compressor cascade flutter tests 20 degrees camber blades, medium and high stagger cascades
D. A. Kilpatrick
;
J. Ritchie
(
1955
)
The effect of compressibility on elevator flutter
D. E. Williams
(
1954
)
Approximate wall corrections for an oscillating swept wing in a wind tunnel of closed circular section
W. E. A. Acum
;
H. C. Garner
(
1955
)
An analysis of N.A.C.A. helicopter reports
R. N. Liptrot
(
1954
)
Full scale measurements of impact loads on a large flying boat part 1 description of apparatus and instrument installation
J.W. McIver
(
1950
)
The theoretical interference velocity on the axis of a two-dimensional wind tunnel with slotted walls
R. C. Tomlinson
(
1954
)
The interaction between shock waves and boundary layers with a note on the effects of the interaction on the performance of supersonic intakes
D. W. Holder et al
(
1955
)
The M.A.E.E. recording accelerometer
D. M. Ridland
;
R. Parker
(
1954
)
A survey of scale effects on the hydrodynamic testing of seaplane models
R. Parker
(
1954
)
Now showing items 3361-3380 of 3498
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