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- W282331710 abstract "Report presenting an investigation in the 300 mph tunnel and on the transonic bump of the high-speed tunnel to determine the feasibility of a self-actuating spoiler as a lateral-control device for a missile with a 60 degree delta wing. Various sizes of plain and cambered spoilers were tested on a 60 degree delta wing through an angle of attack range at low speeds. Results regarding rolling-moment coefficients, yawing-moment coefficients, spoiler actuating times, spoiler rotational-moment coefficients, and spoiler bending-moment coefficients are provided." @default.
- W282331710 created "2016-06-24" @default.
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- W282331710 date "1954-01-28" @default.
- W282331710 modified "2023-09-24" @default.
- W282331710 title "Wind-tunnel investigation at low and transonic speeds of the feasibility of self-actuating spoilers as a lateral-control device for a missile" @default.
- W282331710 hasPublicationYear "1954" @default.
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