Synonyme wurden verwendet für: HYPERSCHALL
Suche ohne Synonyme: keywords:(HYPERSCHALL)

1–20 von 27 Ergebnissen
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    Numerical investigation on the shock wave transition in a three-dimensional scramjet isolator

    Huang, Wei / Wang, Zhen-guo / Pourkashanian, Mohamed et al. | Elsevier | 2010
    Schlagwörter: Hypersonic vehicle

    Effect of geometric parameters on the drag of the cavity flameholder based on the variance analysis method

    Huang, Wei / Pourkashanian, Mohamed / Ma, Lin et al. | Elsevier | 2011
    Schlagwörter: Hypersonic airbreathing engine

    A parametric study on the aerodynamic characteristics of a hypersonic waverider vehicle

    Huang, Wei / Ma, Lin / Wang, Zhen-guo et al. | Elsevier | 2011
    Schlagwörter: Hypersonic waverider vehicles

    Comparison research of two different improved methods in the 2D hypersonic inlet’s design

    Yang, Jun / Luo, Shi-bin / Huang, Wei et al. | SAGE Publications | 2013
    Schlagwörter: Hypersonic inlet

    Novel approach for designing a hypersonic gliding–cruising dual waverider vehicle

    Liu, Jun / Ding, Feng / Huang, Wei et al. | Elsevier | 2014
    Schlagwörter: Hypersonic vehicle

    Influence of surface pressure distribution of basic flow field on shape and performance of waverider

    Ding, Feng / Shen, Chi-bing / Liu, Jun et al. | Elsevier | 2014
    Schlagwörter: Hypersonic vehicle

    Drag reduction mechanism induced by a combinational opposing jet and spike concept in supersonic flows

    Huang, Wei / Liu, Jun / Xia, Zhi-xun | Elsevier | 2015
    Schlagwörter: Hypersonic vehicle

    Comparison between novel waverider generated from flow past a pointed von Karman ogive and conventional cone-derived waverider

    Ding, Feng / Shen, Chi-bing / Liu, Jun et al. | SAGE Publications | 2015
    Schlagwörter: Hypersonic vehicle

    Novel approach for design of a waverider vehicle generated from axisymmetric supersonic flows past a pointed von Karman ogive

    Ding, Feng / Liu, Jun / Shen, Chi-bing et al. | Elsevier | 2015
    Schlagwörter: Hypersonic vehicle

    Drag and heat reduction mechanism in the combinational opposing jet and acoustic cavity concept for hypersonic vehicles

    Huang, Wei / Yan, Li / Liu, Jun et al. | Elsevier | 2015
    Schlagwörter: Hypersonic vehicle

    Novel inlet–airframe integration methodology for hypersonic waverider vehicles

    Ding, Feng / Liu, Jun / Shen, Chi-bing et al. | Elsevier | 2015
    Schlagwörter: Hypersonic waverider vehicle

    Research on the drag reduction performance induced by the counterflowing jet for waverider with variable blunt radii

    Li, Shi-bin / Wang, Zhen-guo / Barakos, George N. et al. | Elsevier | 2016
    Schlagwörter: Hypersonic

    Experimental investigation on drag and heat flux reduction in supersonic/hypersonic flows: A survey

    Wang, Zhen-guo / Sun, Xi-wan / Huang, Wei et al. | Elsevier | 2016
    Schlagwörter: Supersonic/hypersonic flows

    Drag and heat reduction mechanism induced by a combinational novel cavity and counterflowing jet concept in hypersonic flows

    Sun, Xi-wan / Guo, Zhen-yun / Huang, Wei et al. | Elsevier | 2016
    Schlagwörter: Hypersonic flow

    Aerodynamic performance investigation on waverider with variable blunt radius in hypersonic flows

    Li, Shibin / Wang, Zhenguo / Huang, Wei et al. | Elsevier | 2017
    Schlagwörter: Hypersonic flow

    Drag and heat flux reduction mechanism of blunted cone with aerodisks

    Huang, Wei / Li, Lang-quan / Yan, Li et al. | Elsevier | 2017
    Schlagwörter: Hypersonic vehicle

    Multiobjective Design Optimization of Hypersonic Combinational Novel Cavity and Opposing Jet Concept

    Sun, Xi-wan / Huang, Wei / Guo, Zhen-yun et al. | AIAA | 2017
    Schlagwörter: Hypersonic Flows

    Design exploration of combinational spike and opposing jet concept in hypersonic flows based on CFD calculation and surrogate model

    Ou, Min / Yan, Li / Huang, Wei et al. | Elsevier | 2018
    Schlagwörter: Hypersonic reentry vehicle

    Novel design methodology of integrated waverider with drip-like intake based on planform leading-edge definition method

    Chen, Shao-Hua / Liu, Jun / Ding, Feng et al. | Elsevier | 2019
    Schlagwörter: Integrated hypersonic waverider vehicle