Luni-solar perturbations of the orbit of an earth satellite

Some supersonic wind tunnel tests on the fixing of boundary-layer transition using distributed roughnes bands

The orbits of needle satellites

A simple derivation of Lagrange's planetary equations

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

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

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

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

Frictional force measurements on fretted specimens under constant amplitude loading

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

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

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

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

Inspection of gabion structures following august 1986 storm

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

Initial Review of Research into 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

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