A novel approach for inverse design of three-dimensional shock waves under non-uniform flows
H Zhou, Z Jin - Acta Astronautica, 2020 - Elsevier
Traditional osculating axisymmetric flow (OA) theory is widely used in the inverse design of
generalized shock waves. However, this theory is only applicable to uniform incoming flows …
generalized shock waves. However, this theory is only applicable to uniform incoming flows …
Design method for non-axisymmetric generalized internal conical flowfield based on double 3D curved shock waves
H Zhou, Z Jin, N Ge - Aerospace Science and Technology, 2020 - Elsevier
To provide ease of integration design of forebody/hypersonic inward turning inlet as well as
to extend the domain of option for basic flowfield of the inlet, a design method for …
to extend the domain of option for basic flowfield of the inlet, a design method for …
Dual waverider to integrate external and internal flows
Y Li, C Shi, X Zheng, Y You - Journal of Aircraft, 2020 - arc.aiaa.org
This paper proposes a method of integration of internal and external flow called the dual
waverider. A three-dimensional shock structure is designed to simultaneously satisfy the …
waverider. A three-dimensional shock structure is designed to simultaneously satisfy the …
Deficiencies of streamline tracing techniques for designing hypersonic inlets and potential solutions
B Xiong, XQ Fan, Y Wang - Science China Technological Sciences, 2020 - Springer
This work focuses on streamline tracing techniques for designing hypersonic inlets, and two
deficiencies were discovered. Firstly, constriction ratios of stream-traced inlets are …
deficiencies were discovered. Firstly, constriction ratios of stream-traced inlets are …