A simple method is described for calculating the spanwise loading over wing-fuselage combinations. It is based on Multhopp's method, which is extended here to cover wings of finite thickness, large root chords compared ...
Real flow patterns are produced by formally placing a pair of conjugate complex sources at conjugate complex points on the axis of symmetry. These complex singularities are shown to be equivalent to a non-uniform distribution ...
A numerical method has been developed for calculating compressible (inclu- ding transonic) flow past a single aerofoil with an allowance for viscous effects, providing that the boundary layer is fully attached over the ...
The sidestep manoeuvre is investigated in some detail for a slender-wing aircraft by specifying the bank-angle time history and determining the required control angles. The effect of inclusion of the full inertia terms, ...
The subject is introduced by describing the aerodynamic and vibration characteristics of unstalled, supersonic flutter in fan assemblies having part-span shrouds or clappers. It is briefly compared and contrasted with stall ...
F.E. Keates; F.E. Kiddle; R.F. Mousley; D. Gunn(1976)
To assist the development and interpretation of the Concorde Major Fatigue Test a technique for accelerating fatigue testing was evaluated on structural box specimens under combined mechanical and thermal loadings. It is ...
Cumulative fatigue damage has been studied in lugs with and without interference-fit bushes. Fatigue tests have been carried out under constant and variable amplitude loading conditions and local stress measurements have ...
Fatigue tests have been carried out on lugs of BS 2L65 aluminium alloy loaded by steel pins under constant amplitude (CA) and narrow band random (NBR) loading over a range of mean stresses and for different values of ...