Effects of Mach Number on the Performance of a Diverterless Supersonic Inlet

Buzz Cycle Description in an Axisymmetric Mixed-Compression Air Intake

(2016) Mohammad Reza Soltani et al.   AIAA JOURNAL

Flow field and performance analysis of an integrated diverterless supersonic inlet

(2016) J. Masud   AERONAUTICAL JOURNAL

Effects of Boundary-Layer Bleed Parameters on Supersonic Intake Performance

(2015) Mohammad Reza Soltani et al.   JOURNAL OF PROPULSION AND POWER

Effects of Angle of Attack on Inlet Buzz

(2012) Mohammad Reza Soltani et al.   JOURNAL OF PROPULSION AND POWER

An experimental study of buzz instability in an axisymmetric supersonic inlet

(2011) M.R. Soltani et al.   Scientia Iranica

Aerodynamic Design of a Supersonic Inlet with a Parametric Bump

(2009) Sang Dug Kim   JOURNAL OF AIRCRAFT

Numerical study on performance of supersonic inlets with various three-dimensional bumps

(2009) Sang Dug Kim et al.   Journal of Mechanical Science and Technology

Experimental Study of a Mach 3 Bump-Compression Flowfield

(2009) Benjamin J. Tillotson et al.   JOURNAL OF PROPULSION AND POWER