Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Hongwei Chi"'
Publikováno v:
Proceedings of IncoME-VI and TEPEN 2021 ISBN: 9783030990749
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::435df947f19015495ea3e85b875a7cf9
https://doi.org/10.1007/978-3-030-99075-6_79
https://doi.org/10.1007/978-3-030-99075-6_79
Publikováno v:
Journal of Propulsion and Power. 31:1019-1032
The self-ignition characteristics of a solid fuel under supersonic flow have been investigated theoretically and numerically. Time-dependent two-dimensional axisymmetric compressible Navier–Stokes equations and species transport equations are solve
Publikováno v:
Journal of Propulsion and Power. 31:685-693
The specific thrust change rule during the working process of the solid-fuel scramjet combustor was researched using both numerical and experimental methods. A methane-burning vitiated air heater was designed and made to simulate the flight environme
Publikováno v:
Journal of Aerospace Engineering. 28
To research the performance of a solid fuel scramjet combustor, a solid fuel regression rate model was coupled into a quasi-one-dimensional flow equation, and so the flow parameters and fuel regression rate could be calculated together. According to
Publikováno v:
Chinese Journal of Chemical Engineering. 14:464-470
A new type of multi-tube column, in which a novel internal-structure is installed in the bed of random packing, has been invented. The internal-structure reduces the hydraulic radius of the column and adjusts the gas/liquid flow so that the liquid ma
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
The influence on the regression rate of the inlet parameters of a solid fuel (PMMA) under supersonic cross flow has been investigated theoretically and numerically. Based on two-dimensional compressible N-S equations and species transport equations,
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
The characteristics of self-ignition and self-sustained combustion of a solid fuel under supersonic cross flow have been investigated theoretically and numerically. A time dependent two-dimensional, axisymmetric compressible Navier-Stokes equations a
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
The specific thrust level and variation rule of solid fuel scramjet combustor were researched both by numerical and experimental methods. A methane-burning vitiated air heater was designed and made to simulate flight environment of Mach 6 at 25km alt
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Numerical simulations were performed to analyze the performance of solid fuel scramjet (SFSCRJ) operating at Mach 4 to 6, with the primary goal being to investigate the feasibility of low takeover speed for SFSCRJ. The numerical model was created bas