Browsing by Author "J. Callinan"

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Experiments at M = 1.41 on a thin, conically-cambered elliptic cone of 30 degrees semi-vertex angle

E. W. E. Rogers; V. G. Quincey; J. Callinan (1961)

Pressure-plotting and strain-gauge balance tests have been made at a Mach number of 1.41 on a conically cambered cone of 30° semi-vertex angle, and with a ratio of the major to the minor axis of its cross-section equal to ...
Experiments at M0 = 4.03 on two families of pressure-plotting wing-and-half-cone combinations

E. W. E. Rogers; J. L. Attridge; Miss A. G. J. Macdonald; J. Callinan (1964)

Tests have been made at a Mach number of 4.03 and Reynolds number of 3.4 million on two families of models, consisting of delta wings with underslung half-Cone bodies. The wing sweepback angles were 75° and 80°, and the ...
Experiments on two-dimensional base flow at subsonic and transonic speeds

J. F. Nash; V. G. Quincey; J. Callinan (1963)

A report is presented of a series of experiments aimed at an investigation of the fundamental mechanisms of the flow behind an isolated blunt-trailing-edge section, and a rearward-facing step, at subsonic and transonic ...

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