SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVER-EXPANDED CONICAL EXHAUST NOZZLES

Truncated Perfect Nozzles in Optimum Nozzle Design

Jörgen Ahlberg, Steven Hamilton, D. MIGDAL et al. · ARS journal · 1961 · 75 citations

Compressible Flow, Engineering, Aerospace Engineering +14

Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause Separation

Geoffrey Michael Gadd · Journal of the aeronautical sciences. [REQUEST TITLE] · 1953 · 65 citations

Unsteady Flow, Engineering, Physics +6

Investigation of Supersonic Flow Separation in Nozzles

R. P. Fraser, P. Eisenklam, David Wilkie · Journal of Mechanical Engineering Science · 1959 · 17 citations

Unsteady Flow, Compressible Flow, Engineering +4

Editors

Jet propulsion · 1954 · 16 citations