Browsing Aeronautical Research Council Reports & Memoranda by Author "V. G. Quincey"

Now showing items 1-3 of 3

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 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 ...
Tests at transonic speeds on wings with wedge sections and sweep varying between 0 degree and 60 degrees

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

Tests have been made in the N.P.L. 18 in. by 14 in. High-Speed Tunnel at stream Mach numbers between 0.6 and 1.2 on two finite wings of identical planform and having single-wedge and double-wedge sections of 14% and 7% ...

Search AERADE