Browsing by Author "P. E. Watts"

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A wind tunnel investigation of the longitudinal and lateral aerodynamic characteristics of a Canard Aircraft model Part 1 Tests at M = 1.04 and M = 2.02 Part 2 Tests at M = 2.47

P. E. Watts; L. J. Beecham; D. A. Treadgold (1959)

PART I. Tests were made in the Royal Aircraft Establishment No. 19 (18 in. x 18 in.) supersonic wind tunnel to measure the overall normal and side forces, rolling, pitching and yawing moments on a typical canard aircraft ...

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