airscrew

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Airscrew

The diameter of an airscrew may be as much as 6-7 m. The blades of airscrews are made from wood, Duralumin, steel, and composition materials. At air speeds between 600 and 800 km/hr, the efficiency of an airscrew varies from 0.9 to 0.8 respectively. Efficiency declines at higher speeds as a result of the compressibility of air. The main way of reducing the power loss owing to the compressibility of the air is to use thin-profile blades with low camber.

Figure 1. Profile of an airscrew blade (with velocity and force vectors): (α) angle of attack, (φ) blade angle,(V) forward speed of screw, (ωr) peripheral velocity of a blade section, (w) additional airstream velocity at blade section caused by the screw, (ΔR) aerodynamic force, (ΔP) thrust, (ΔQ) resistance to the rotation of a blade section. The dotted line indicates the chord of the profile.

The idea of the airscrew was suggested in 1475 by Leonardo da Vinci, but it was first used to generate thrust by M. V. Lomonosov in 1754 in a model of a meteorological research instrument. By the mid-19th century, marine propellers, operating in the same way as airscrews, were in use on ships. In the 20th century airscrews have come to be used on dirigibles, airplanes, helicopters, aerosleighs, air-cushion vehicles, and so on. The methods of aerodynamics calculation and design of airscrews are based on extensive theoretical and practical research. In the period from 1892 to 1910 the Russian research engineer and inventor S. K. Dzhevetskii developed the theory of the isolated blade section, which was further developed in 1910-11 by the Russian scientists B. N. Iur’ev and G. Kh. Sabinin. From 1912 to 1915, N. E. Zhukovskii established the vortex theory, which gives a clear physical representation of the operation of the airscrew and other bladed devices and establishes the mathematical correlation between the forces, velocities, and geometrical parameters of devices of this type. A significant role in the further development of this theory and its engineering applications and in research into the strength of airscrews was played by V. P. Vetchinkin and his coworkers. The theory of the optimum screw with a finite number of blades was established by the German scientist A. Betz (1919) and the British scientist S. Goldstein (1929) and has been further developed in the work of Soviet scientists. In 1956 the Soviet scientist G. I. Maikopar extended the vortex theory of airscrews to the helicopter rotor.

REFERENCES

Zhukovskii, N. E. Poln. sobr. soch., vol. 6. Moscow-Leningrad, 1937.
Vetchinkin, V. P., and N. N. Poliakov. Teoriia i raschet vozdushnogo grebnogo vinta. Moscow, 1940.
Maikopar, G. I., A. M. Lepilkin, and D. V. Khalezov. “;Aerodinamicheskii raschet vintov po lopastnoi teorii.” Tr. Tsentr. aerogidrodinamicheskogo in-ta, 1940, fasc. 529.
Aleksandrov, V. L. Vozdushnye vinty. Moscow, 1951.
Issledovaniia vozdushnykh vintov. Moscow, 1969.(Materialy k istorii TsAGL)

B. P. BLIAKHMAN

airscrew

A propeller. The term is no longer in use.
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