Implementation of various-fidelity methods for viscous effects modeling on the design of a waverider-Reference-Cited by-同舟云学术

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Implementation of various-fidelity methods for viscous effects modeling on the design of a waverider

Published:2023-02 Issue: Volume:133 Page:108141
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Bliamis Chris,Menelaou Constantinos^ORCID,Yakinthos Kyros^ORCID

Funder

Hellenic Foundation for Research and Innovation

Aristotle University of Thessaloniki

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference57 articles.

1. The aerodynamic design of aircraft;Kuchemann,1978

2. Aerodynamic Problems of Manned Space Vehicles;Nonweiler,1958

3. On the conceptual design of waverider forebody geometries;Kontogiannis,2015

4. Dual waverider concept for the integration of hypersonic inward-turning inlet and airframe forebody;You,2009

5. Analysis of cone-derived waverider by hypersonic small-disturbance theory;Rasmussen,1990

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1. Numerical study on hypersonic aerodynamic characteristics of the high-pressure capturing wing configuration with wing dihedral;Aerospace Science and Technology;2023-12

2. A conjugate numerical model for the thermal analysis of the regenerative cooling of an X-51A-like aircraft;Physics of Fluids;2023-09-01

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