Download PDF by D.R. Philpott, R.H. Barnard: Aircraft Flight: A description of the physical principles of

By D.R. Philpott, R.H. Barnard

ISBN-10: 0273730983

ISBN-13: 9780273730989

Airplane Flight offers exact actual, instead of mathematical, descriptions of the foundations of airplane flight. This renowned textual content supplies mechanical engineering and aeronautical engineering scholars an invaluable creation to the topic. The fourth variation has been up-to-date to incorporate very important contemporary advancements similar to unmanned air cars and the low orbit space-plane

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Extra info for Aircraft Flight: A description of the physical principles of aircraft flight

Example text

It should be noted that the description above applies to conventional helicopters. Various alternative rotor mechanisms have been tried, including ones with tilting shafts. Since the rotor provides thrust, lift and the primary means of control, the helicopter can be seen as a good example of a radical departure from Cayley’s classical aeroplane, where each component serves only one specific purpose. The helicopter also suffers from other problems stemming from the differences in the relative airflow velocities on the advancing and retreating blades.

There are several important consequences of this deflection. Firstly, as we can see from the diagrams, the angle of attack relative to the modified local airstream direction, is reduced. This reduction in effective angle of attack means that less lift will be generated, unless we tilt the wing at a greater angle to compensate. The second, and more important consequence may be explained by further reference to Fig. 8. QXD 14/9/09 15:20 Page 44 44 WINGS Fig. 8 The effect of downwash on lift and drag (a) Lift force in two-dimensional flow with no downwash effect (b) Downwash changes local approach flow direction.

26 On the so-called rigid rotor design, flapping is provided by flexible members and compliant joints which replace the hinges of older designs. Note the compactness and simplicity relative to the Kamov design shown in Fig. 25 Fig. 27 Helicopter in forward flight The blades are caused to flap up at the rear by use of the cyclic pitch control. QXD 14/9/09 15:18 Page 31 LIFT FROM ROTATING WINGS When a helicopter flies forwards, the relative air speed on the advancing blade side will be greater than on the retreating side.

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Aircraft Flight: A description of the physical principles of aircraft flight by D.R. Philpott, R.H. Barnard


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