Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers

Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition

Dean R. Chapman, D. M. Kuehn, H. K. Larson · University of North Texas Digital Library (University of North Texas) · 1958 · 639 citations · Full text

Engineering, Aerospace Engineering, Physics +17

Recent research progress on unstart mechanism, detection and control of hypersonic inlet

Juntao Chang, Nan Li, Kejing Xu et al. · Progress in Aerospace Sciences · 2016 · 266 citations

Engineering, Aerospace Engineering, Process Control +12

Starting characteristics of supersonic inlets

David Van Wie, F. KWOK, Ray Walsh · 32nd Joint Propulsion Conference and Exhibit · 1996 · 216 citations

Engineering, Aerospace Engineering, Computational Fluid Dynamics +14

Preliminary Investigation of Supersonic Diffusers

Arthur Kantrowitz, Coleman duP. Donaldson · University of North Texas Digital Library (University of North Texas) · 1945 · 201 citations · Full text

Engineering, Aerospace Engineering, Physics +13

Turbulent boundary-layer separation in front of a forward-facing step.

E. E. Zukoski · AIAA Journal · 1967 · 190 citations

Engineering, Aerospace Engineering, Physics +17