Zobrazeno 1 - 10
of 24
pro vyhledávání: '"Huacheng Yuan"'
Publikováno v:
Aerospace, Vol 9, Iss 12, p 811 (2022)
The Reynolds number effect induced by model scaling and inflow conditions will affect the aerodynamic and starting characteristics of a two-dimensional hypersonic inlet. This effect is investigated through a numerical simulation method. First, the nu
Externí odkaz:
https://doaj.org/article/913834f068b94a04ae92f0145eb44c59
Publikováno v:
Aerospace, Vol 9, Iss 11, p 685 (2022)
As hypersonic vehicles are highly integrated, a multifidelity simulation method based on a commercial solver is developed to reduce simulation time for such vehicles and their propulsion systems. This method is characterized by high-level fidelity nu
Externí odkaz:
https://doaj.org/article/eaf5b8ad025d4027a9336d8b4d8d3ac0
Publikováno v:
Propulsion and Power Research, Vol 4, Iss 3, Pp 141-149 (2015)
A turbine based combined cycle (TBCC) propulsion system uses a turbine-based engine to accelerate the vehicle from takeoff to the mode transition flight condition, at which point, the propulsion system performs a “mode transition” from the turbin
Externí odkaz:
https://doaj.org/article/766c1fc33acd4e62beeb81dcd46cb114
Publikováno v:
Journal of Aerospace Engineering. 36
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f92bb2e0c7a56610cfb90f3f738b6b15
https://doi.org/10.1061/jaeeez.aseng-4249
https://doi.org/10.1061/jaeeez.aseng-4249
Publikováno v:
International Journal of Turbo & Jet-Engines.
Based on the flow field characteristics of the missile body, an integrated design method for missile and inlet with two side layout is proposed under asymmetric inflow. The result of numerical simulation shows that shock waves hit on cowl lip on the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d5e64006ed5a786c6176ac1a3905dc5a
https://doi.org/10.1515/tjj-2022-0076
https://doi.org/10.1515/tjj-2022-0076
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 235:1763-1778
Design of a supersonic inlet with double S-bend diffuser was developed. Numerical simulation and wind tunnel experiment were carried out to investigate the aerodynamic performance and variable geometric rules of the inlet. The result indicates that t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75a18746185c208dc5abae00383a9d38
https://doi.org/10.1177/0954410020983981
https://doi.org/10.1177/0954410020983981
Publikováno v:
International Journal of Turbo & Jet-Engines.
The design of a two-dimensional variable geometry inlet which applied to a tandem type turbine-based combined cycle (TBCC) propulsion system was investigated in the present paper through three-dimensional simulations and wind tunnel tests. The operat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::95ad07953a30d982861c1495d10aa63f
https://doi.org/10.1515/tjj-2021-0024
https://doi.org/10.1515/tjj-2021-0024
Publikováno v:
International Journal of Turbo & Jet-Engines.
Design and aerodynamic performance analysis of a variable geometry axisymmetric inlet was carried out for tandem scheme turbine-based combined cycle (TBCC) propulsion system. The operation Mach number of the inlet was between 0 and 4. The design poin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3903b58147ed04ace94767ba2a282a4a
https://doi.org/10.1515/tjeng-2020-0030
https://doi.org/10.1515/tjeng-2020-0030
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Publikováno v:
Aerospace Science and Technology. 118:107008
Aiming at the problem of starting and inlet-engine matching of axisymmetric variable geometry inlet with complex structure, a novel design concept of axisymmetric inlet is proposed based on controllable bleed slots switch. The laws of the typical geo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3cdfbda9464c2a69b653fd66358a8db2
https://doi.org/10.1016/j.ast.2021.107008
https://doi.org/10.1016/j.ast.2021.107008