Inverse design of a curved wall compression hypersonic inlet based on Genetic Algorithms

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2011, 32 (5)： 601-605   

Shock wave oscillation for outlet-closed ramjet inlet

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2011, 32 (5)： 606-610   

Experiment of the static pressure on the rotating blade surface in an axial compressor

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2011, 32 (5)： 611-616   

Experiment of the flow in a cover-plate pre-swirl system

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2011, 32 (5)： 654-657   

Reliability and multidisciplinary design optimization for turbine blade based on single-loop method

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2011, 32 (5)： 658-663   

Investigation into effects of interaction among suction flow,shock wave and separation flow for a transonic compressor cascade

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2011, 32 (5)： 664-669   

Quasi-steady model of moving droplet evaporation process under low frequency pressure oscillation

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2011, 32 (5)： 670-675   

Numerical simulation on trapped-vortex combustor model for ramjet engine

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2011, 32 (5)： 676-679   

Experimental investigation of strut-cavity flameholder technology in liquid hydrocarbon fueled scramjet combustor

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2011, 32 (5)： 680-683   

Flame stabilizing mechanism of recirculation-zone of cavity flameholder

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2011, 32 (5)： 684-689   

Calculation and analysis of fuel concentration at the rear of spray injecting element

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2011, 32 (5)： 690-693   

Numerical investigations of the fuel injection ring design in ramjet

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2011, 32 (5)： 694-697   

Effects of delamination of needled preform on thermal insulation of C/C-SiC chamber

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2011, 32 (5)： 698-705   

Effect of rotation on film cooling under different inflow conditions

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2011, 32 (5)： 706-712   

A model to analyze the film cooling characteristics of a ramjet combustor

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2011, 32 (5)： 713-716   

Analysis of local buckling distortion and deformation of a ramjet combustor shell in a structural and thermal experiment

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2011, 32 (5)： 717-721   

State space modeling based on QPSO hybrid method for aero-engines

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2011, 32 (5)： 722-727   

A new method for detecting the aging property of HTPB solid propellant

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2011, 32 (5)： 728-731   

Effect of propellant temperature on the specific impulse liquid apogee engine

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2011, 32 (5)： 732-736   

Optimal design and examination study of biaxial tensile specimens for solid propellant

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2011, 32 (5)： 737-740   

Numerical study on characteristics of aero-acoustics pilot wind tunnel fan section

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2011, 32 (5)： 741-745   

Design of multi-detonator pulse detonation engine with fuel/air mixture radial filling

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2011, 32 (5)： 746-750