Optimization of scramjet inlet based on temperature and Mach number of supersonic combustion

Experimental study on ejector-to-ramjet mode transition in a divergent kerosene-fueled RBCC combustor with low total temperature inflow

(2020) Lei Shi et al.   AEROSPACE SCIENCE AND TECHNOLOGY

Buzz evolution process investigation of a two-ramp inlet with translating cowl

(2018) Wen Shi et al.   AEROSPACE SCIENCE AND TECHNOLOGY

Effects of the aerothermoelastic deformation on the performance of the three-dimensional hypersonic inlet

(2018) Kun Ye et al.   AEROSPACE SCIENCE AND TECHNOLOGY

An aerothermodynamic design optimization framework for hypersonic vehicles

(2018) Simone Di Giorgio et al.   AEROSPACE SCIENCE AND TECHNOLOGY

Experimental Investigation of Brazilian 14-X B Hypersonic Scramjet Aerospace Vehicle

(2017) João Felipe de Araujo Martos et al.   International Journal of Aerospace Engineering

Preliminary analysis of scramjet engines based on engineering models

(2015) Tiago C. Rolim et al.   AEROSPACE SCIENCE AND TECHNOLOGY

A new approach for the design of hypersonic scramjet inlets

(2012) N. Om Prakash Raj et al.   PHYSICS OF FLUIDS