Exhaust Plume Temperature Effects on Nozzle Afterbody Performance Over the Transonic Mach Number Range / C.E. Robinson and M.D. High..C E Robinson, M Dean High & 3 more1974EN
Evaluation of Reynolds Number and Tunnel Wall Porosity Effects on Nozzle Afterbody Drag at Transonic Mach NumbersC E Robinson, Aro & 2 more1976EN