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Showing 5 out of a total of 5 results for community: Aeronautical Research Council.
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Wind tunnel measurements of the far-field pressures due to some lifting, slender delta wings
T. A. Cook
(
1965
)
Supersonic wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft part 1 M = 1.4 to 2.0 part 2 M = 2.0 to 2.7
C. R. Taylor
;
T. A. Cook
(
1965
)
Wind tunnel tests at mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on a slender, cambered ogee wing
T. A. Cook
(
1965
)
Wind tunnel measurements at mach numbers up to 2.80 of the effects of gulling on the longitudinal and lateral stability and drag of a cambered, slender ogee wing
T. A. Cook
(
1965
)
Wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft with rectangular, wedge intakes at mach numbers from 2.0 to 2.7
T. A. Cook
(
1965
)
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T. A. Cook (5)
C. R. Taylor (1)
Date Issued
1965 (5)