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- W191013163 abstract "A design is considered in which the wind tunnel is an integral part of a system suitable for the simulation of the behaviour of aircraft and missiles in flight. The static aerodynamic loads on a wind tunnel model, mounted on a conventional quadrant support, are measured and combined with continuously computed gravitational, inertial and aerodynamic damping loads, the model orientation to the flight path being correctly maintained throughout. The computer elements comprise a small analogue unit for the on-line correction of the wind tunnel data, and a D.D.A. unit consisting of commercially available CORSAIRs for the kinematic simulation and wind tunnel control." @default.
- W191013163 created "2016-06-24" @default.
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- W191013163 date "1962-11-30" @default.
- W191013163 modified "2023-09-27" @default.
- W191013163 title "Proposals for an integrated wind tunnel-flight dynamics simulator systems" @default.
- W191013163 hasPublicationYear "1962" @default.
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