Normal force and pitching moment have been measured on a number of cone cylinder combinations at a Mach number of 3.98 in the 3 ft x 4 ft High Supersonic Speed Tunnel. The results are presented graphically. Comparison is ...
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 ...