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Showing 10 out of a total of 33 results for collection: Aeronautical Research Council Reports & Memoranda.
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Flight tests at high mach number on E28/39 W4041 (single-engined jet-propelled aircraft)
A. W. Thom
;
F. Smith
;
J. Brotherton
(
1945
)
Tank Tests on a Hull with the Main Step Faired in Planform and Elevation
D. I. T. P. Llewelyn-Davies
(
1945
)
The Ideal Drag Due to a Shock Wave. Parts I and II
C. N. H. Lock
(
1945
)
Flight Tests on "King Cobra" FZ.440 to investigate the Practical Requirements for the Achievement of Low Profile Drag Coefficients on a "Low Drag" Aerofoil
F. Smith
;
D. J. Higton
(
1945
)
A theoretical investigation of the response of a highspeed aeroplane to the application of ailerons and rudder
K. Mitchell
;
A. W. Thorpe
;
E. M. Frayn
(
1945
)
A theoretical calculation of the reduction in drag obtainable by ejector action of the exhaust gases when mixed with the cooling air-flow of a typical air-cooled engine
A. B. P. Beeton
(
1945
)
Notes on the design of converging channels
S. Goldstein
(
1945
)
Theoretical velocity distribution in a high-speed tunnel contraction
M. Jones
;
P. Bright
(
1945
)
An experimental investigation into the suitability of a corrugated construction wing for a laminar-flow aerofoil
J. C. King
(
1945
)
The increase in thrust obtainable from a power plant installation using the cooling-air as a propulsive jet
A. B. P. Beeton
(
1945
)
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Author
A. B. P. Beeton (2)
E. M. Frayn (2)
F. Smith (2)
J. C. King (2)
K. Mitchell (2)
M. J. Lighthill (2)
M. Jones (2)
A. H. Bell (1)
A. W. Thom (1)
A. W. Thorpe (1)
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Date Issued
1945 (33)