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Showing 5 out of a total of 5 results for community: Aeronautical Research Council.
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Use of camber and twist to produce low-drag delta or swept-back wings, without leading-edge singularities, at supersonic speeds
G. M. Roper
(
1958
)
Some applications of the lamé function solutions of the linearised supersonic flow equations. Part I. Finite swept-back wings with symmetrical sections and rounded leading edges. Part II. Cambered and twisted wings
G. M. Roper
(
1951
)
Calculation of the effect of camber and twist on the pressure distribution and drag on some curved plates at supersonic speeds
G. M. Roper
(
1950
)
Drag reduction of thin wings at supersonic speeds, by the use of camber and twist
G. M. Roper
(
1957
)
Formulae for calculating the camber surfaces of thin swept-back wings of arbitrary plan-form with subsonic leading edges, and specified load distribution
G. M. Roper
(
1959
)
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G. M. Roper (5)
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1959 (1)
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1951 (1)
1950 (1)