Two programmes are presented in I.C.L. FORTRAN, for the pressure distribution on the surface of an arbitary body of revolution in axisymmetric, incompressible flow. One programme evaluates the pressure distribution on an ...
Four models of an aircraft configuration with a 55 degree swept wing were flown at Mach numbers between 0.9 end 1.4, at Reynolds numbers up to 10 million and lift coefficients between zero and 0.5. Measurements of the ...