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Engine Cowling with Special Reference to the Air-Cooled Engine

Published online by Cambridge University Press:  28 July 2016

J. D. North
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Extract

In the earliest stages of the development of the aeroplane the speed range obtainable was small, flight occurred only at fairly high lift coefficients, and induced drag was the predominant component of total resistance, hence successful flight depended on the achievement rather of minimum weight, minimum wing loading and maximum engine power than on the achievement of minimum possible parasite resistance.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 38 , Issue 283 , July 1934, pp. 565 - 612
Copyright
Copyright © Royal Aeronautical Society 1934

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References

1. Gibson.Google Scholar
2. Deperdussin, French Patents Nos. 444619, 447788 (1912).Google Scholar
3. N.A.C.A. Report No. 313.Google Scholar
4. Pye, , The Principles of Air Cooling. Aircraft Engineering, Feb., March, April, 1933.Google Scholar
5. Wood, McKinnon, Engine Cooling Research. Journal R.Ae.S., September, 1933.Google Scholar
6. Junkers, , British Patents Nos. 147003, 148889.Google Scholar
7. Townend, , British Patent No. 320131.Google Scholar
9. Boulton & Paul, Wind Channel.Google Scholar
10. Fedden, , Research on Low Drag Cowling. Aeronautical Engineering, September, 1933.Google Scholar
11. N.A.C.A. Report No. 414.Google Scholar
12. Boulton & Paul, Wind Channel.Google Scholar