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L. M. Sheppard

  • A method for determining the maximum thickness position for minimum wave drag for wings with supersonic edgesA method for determining the maximum thickness position for minimum wave drag for wings with supersonic edges
  • Estimation of the interference wave drag between separated components of a wing-body combinationEstimation of the interference wave drag between separated components of a wing-body combination
  • Experimental evidence on the transonic and supersonic similarity laws for the wave drag of non-lifting wingsExperimental evidence on the transonic and supersonic similarity laws for the wave drag of non-lifting wings
  • Improving the accuracy of pressure distributions in linearised supersonic wing theoryImproving the accuracy of pressure distributions in linearised supersonic wing theory
  • Methods for determining the wave drag of non-lifting wing-body combinationsMethods for determining the wave drag of non-lifting wing-body combinations
  • Some free flight tests on the sonic area rule and wing-body wave dragSome free flight tests on the sonic area rule and wing-body wave drag
  • Supersonic estimation of the wing incidence equivalent to a camber distributionSupersonic estimation of the wing incidence equivalent to a camber distribution
  • Supersonic wing-body interference: wing and body at zero incidenceSupersonic wing-body interference: wing and body at zero incidence
  • Transonic drag tests of 32 wings having R.A.E. 104 sectionsTransonic drag tests of 32 wings having R.A.E. 104 sections