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Rotary Derivatives of a Delta Wing at Supersonic Speeds

Published online by Cambridge University Press:  28 July 2016

A. Robinson
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Summary

The rotary derivatives of a Delta wing pitching or rolling at supersonic speed are obtained in addition to the lift curve slope first given in an earlier investigation.

Type
Research Article
Information
The Aeronautical Journal , Volume 52 , Issue 455 , November 1948 , pp. 735 - 752
Copyright
Copyright © Royal Aeronautical Society 1948

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References

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