Horizontal control effector sizing for supersonic transport aircraft... locations at the approach ight condition of a supersonic transport aircraft, dynamic constraints may be more restrictive than the static ones
Printed in great britain 1352ð2310/98 $19.00#0.00pii: s1352±2310(97)00489±5 editorial research on the effects of aircraft and spacecraft upon the atmosphere...chemical or meteorological changes in the climatic state of the atmosphere was discussed intensively within studies performed in the early 1970s when plans to build a ßeet of supersonic transport aircraft (SST) were under discussion (Johnston, 1971; Crutzen, 1971; CIAP, 1975)....
Minimum mass sizing of a large low-aspect ratio airframe for flutter-free performanceA procedure for sizing an airframe for flutter-free performance is demonstrated on a large, flexible supersonic transport aircraft....
Using numerical simulations to explore top-mounted propulsion on a conceptual commercial supersonic transport aircraftReynolds Averaged Navier-Stokes (RANS) simulations were performed on an N+2 conceptual commercial supersonic transport aircraft to explore the possibility of relocating the engines from below the wings to above the wings in order to capitalize upon potential noise shielding...
