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The Lotz Method for Calculating the Aerodynamic Characteristics of Wings

Published online by Cambridge University Press:  28 July 2016

Extract

The method generally used in England for calculating the aerodynamic characteristics of wings is that suggested by Glauert (1), in which the circulation across the span of the wing is represented by a Fourier series. On account of the form of the series, certain difficulties arise which make the calculation very tedious when more than about four points along the semi-span are considered.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1934

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References

References

1. Glauert, H.. “ The Elements of Aerofoil and Airscrew Theory,” Chapter XI.Google Scholar
Strength Calculations Handbook (A.P. 970), Chapter VIII.Google Scholar
2. Lotz, I.. “ Berechnung der Auftriebsverteilung beliebig geformter Fluegel.” Z.F.M., 1931, p. 189.Google Scholar
Koning, and Boelen, . “ Aerodynamische Eigenschaften der Quasi-Trapezfluegel mit verschiedener Breite des prismatischen Teiles.” Z.F.M., 1933, p. 43.Google Scholar
Hueber, . “ Die Aerodynamischen Eigenschaften von Doppeltrapezfoermigen Tragfluegeln.” Z.F.M., 1933, p. 249 and p. 269.Google Scholar
Hueber, . “ Der Verwundene Trapezfluegel.” Z.F.M., 1933, p. 307.Google Scholar
3. Vladea, Joan. “ Ueber den Einfluss des Rumpfes (Gondeln) auf einige aereodynamische Eigenschaften des Fluegels.” Z.F.M., 1933, p. 555.Google Scholar
4. Hermann, L.. Archiv fuer die gesamte Physiologie (Pflueger) 1890, p. 45.CrossRefGoogle Scholar
Lohmann, . “ Harmonische Analyse zum Selbstunterricht.” Fischers Medizinische Buchhandlung, Leipzig, 1921.Google Scholar
5. R. & M. 1095. “ Theoretical Relationships for an Aerofoil with Hinged Flap.”Google Scholar