A technique for the wind tunnel simulation of store release at high speeds

von Beecham, L. J.
Veröffentlicht 1966

The hemispherical, differential pressure yawmeter at supersonic speed

von Beecham, L. J.
Veröffentlicht 1961

Some aerodynamic considerations of the flight characteristics of towing systems using long towlines at high speeds

von Pierce, D.
Veröffentlicht 1972

Tests at M=1.04 and M=2.02

von Watts, P. E.
Veröffentlicht in A wind tunnel investigation of the longitudinal and lateral aerodynamic characteristics of a canard aircraft model (1962)

An approximate analysis of the non linear lateral motion of a slender aircraft (HP 115) at low speeds

von Ross, A. Jean
Veröffentlicht 19701971

Some notes on an approximate solution for the free oscillation characteristics of non linear systems typified by x͏̈+F(x,ẋ)0

von Beecham, L. J.
Veröffentlicht 19691971

Static and dynamic response of a design of a differential pressure yawmeter at supersonic speeds

von Beecham, L. J.
Veröffentlicht 1958

Exploratory tests on a thin delta wing in the flow field of a rectangular foreplane at Mach number 1.8

von Igglesden, M. S.
Veröffentlicht 1961

Proposals for an integrated wind tunnel-flight dynamics simulator system

von Beecham, L. J.
Veröffentlicht 1965

A wind tunnel investigation of the longitudinal and lateral aerodynamic characteristics of a canard aircraft model

Veröffentlicht 19591962