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Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê
William Mulcay1979
Páginas: 692
Género: Ground simulators
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The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models
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Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊
William Mulcay
1980
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Applications and requirements for real-time simulators in ground-test facilities
Dale J. Arpasi
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Performance testing of a main rotor system for a utility helicopter at 1/4 scale
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1982
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