John R. Carlson
A nozzle internal performance prediction method
Comparison of experimental surface pressure with theoretical predictions on twin two-dimensional convergent-divergent nozzles
Computational prediction of isolated performance of an axisymmetric nozzle at Mach number 0.90
Integration effects of pylon geometry on a high-wing transport airplane
Integration effects of pylon geometry on a high-wing transport plane
Personal injury damages
Two-dimensional converging-diverging rippled nozzles at transonic speeds