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HYPERSCHALL
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keywords:(HYPERSCHALL)
Backpressure unstart detection for a scramjet inlet based on information fusion
Effects of boundary-layers bleeding on performance parameters of hypersonic inlets
Mathematical modeling and rapid recognition of hypersonic inlet buzz
Real-time unstart prediction and detection of hypersonic inlet based on recursive Fourier transform
Real-time unstart prediction and detection of hypersonic inlet based on recursive Fourier transform
Operation pattern classification of hypersonic inlets
Mathematical modeling and characteristic analysis of scramjet buzz
Effects of wall cooling on performance parameters of hypersonic inlets
Numerical study on hypersonic nozzle-inlet starting characteristics in a shock tunnel
Hypersonic vehicle terminal velocity improvement considering ramjet safety boundary constraint
Performance optimization of hypersonic inlets with pulse periodic energy addition
Dynamic Characteristics of Combustion Mode Transitions in a Strut-Based Scramjet Combustor Model
Unstart Margin Characterization Method of Scramjet Considering Isolator–Combustor Interactions
Experimental Investigation of Hysteresis Phenomenon for Scramjet Engine
An Estimation Method for Scramjet Inlet Mach Number and Mass Flow Rate Based on Deep Learning
Mechanism Study on Local Unstart of Hypersonic Inlet at High Mach Number
Mechanism and Prediction for Occurrence of Shock-Train Sharp Forward Movement
Numerical Investigation of Local Resistance to Backpressure in Hypersonic Inlet with Suction