Review of initial experiments using the Hawk model, dynamic rig facility and the CED1401 digital data acquisition equipment

Measurement of the Longitudinal Static Stability and the Moments of Inertia of a 1/12th Scale Model of a B.Ae Hawk

Preliminary Studies for Aircraft Parameter Estimation Using Modified Stepwise Regression

Third Quarterly Report on the Application of Modified Stepwise Regression for the Estimation of Aircraft Stability and Control Parameters

Second Quarterly Report on the Application of Modified Stepwise Regression for the Estimation of Aircraft Stability and Control Parameters

Initial Review of Research into the Application of Modified Stepwise Regression for the Estimation of Aircraft Stability and Control Parameters

A Summary Report on an Experimental Investigation into Methods for Quantifying Hang Glider Airworthiness Parameters

A progress report on a programme of research into the aerodynamics, stability and control characteristics ol a combat aircraft having a forward swept wing

A Technique for Optimising the Aerodynamic Design of a Generalised Combat Aircraft with Forward Swept Wings for the purposes of Stability and Control Investigation

The effect of supplementary protectives on the fatigue performance of a riveted lap joint

Odd zonal harmonics in the geopotential, from analysis of 28 satellite orbits

Frictional force measurements on fretted specimens under constant amplitude loading

Wind tunnel measurements of the far-field pressures due to some lifting, slender delta wings

Wind tunnel tests at mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on a slender cambered ogee wing

Wind tunnel measurements at mach numbers up to 2.80 of the effects of gulling on the longitudinal and lateral stability and drag of a cambered, slendered ogee wing

Supersonic wind tunnel measurements of the loads and internal pressure distributions on internally parallel ducts at incidence

Determination of the even harmonics in the earth's gravitational potential

The contraction of satellite orbits under the influence of air drag: Part IV: with scale height dependent on altitude

A simple derivation of Lagrange's planetary equations

The orbits of needle satellites