117 resultados para Stalling (Aerodynamics)


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Includes bibliographical references.

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Mode of access: Internet.

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Reproduced from typewritten copy.

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Reproduced from typewritten copy.

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"It is shown that adequate means are available for calculating inviscid direct and induced pressures on simple axisymmetric bodies at zero angle of attack. The extent to which viscous effects can alter these predictions is indicated. It is also shown that inviscid induced pressures can significantly affect the stability of blunt, two-dimensional flat wings at low angles of attack. However, at high angles of attack, the inviscid induced pressure effects are negligible."

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Reproduced from type-written copy.

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Description based on: RM no. A6G24 (May 12, 1947); title from cover.

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"AEDC TDR-62-54. Program area 750A. AFSC project 4773. Contract no. AF40(600)-804."

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Mode of access: Internet.

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"First three editions comprising 2400 copies were published between Dec. 1934 and June 1939."

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"Task 9R99-01-005-04. Contract DA 44-177-TC-710."