Results 61 to 70 of about 8,165 (229)

Numerical Investigation of Chemically Reacting Rarefied Hypersonic Flows Over A Backward-Facing Step [PDF]

, 2021
Arjun Singh
openalex   +1 more source

Combustion synthesis of ultra‐high temperature ceramics: Review

International Journal of Applied Ceramic Technology, Volume 22, Issue 6, November/December 2025.
Abstract Novel and future‐oriented aerospace, energy, transportation, and other industrial technologies require materials capable of operating at temperatures above 2000°C. Ultra‐high temperature ceramic materials (UHTCs), based on carbides, borides, carbonitrides, and nitrides of transition metals—many with melting points exceeding 3000°C—possess the ...
Alexander S. Mukasyan, Alexander S. Rogachev   +1 more
wiley   +1 more source

Micro-Ramps for Hypersonic Flow Control

Micromachines, 2012
Shock/boundary layer interaction (SBLI) is an undesirable phenomenon, occurring in high-speed propulsion systems. The conventional method to manipulate and control SBLI is using a bleed system that involves the removal of a certain amount of mass of the ...
Konstantinos Kontis, Azam Che-Idris, Hossein Zare-Behtash, Mohd R. Saad   +3 more
doaj   +1 more source

Starting Process of a Double-Throat Ludwieg Tube Tunnel and the Extension of Its Effective Running Time

气体物理
The Ludwieg tube wind tunnel serves as a crucial testing ground for fundamental studies of hypersonic aerodynamics. However, the quick-opening valve-started hypersonic Ludwieg tube wind tunnel has been affected by the quick-opening valve for a long time,
Chuangchuang LI, Zhiyuan LI, Zhenhui ZHANG, Jie Wu   +3 more
doaj   +1 more source

A review on the development of large-scale detonation-driven shock tunnels and the application in hypersonic flow tests [PDF]

International Journal of Fluid Engineering
With the boom in deep space exploration by China since the beginning of the 21st century, the demand for high-enthalpy hypersonic shock tunnels has continued to increase.
Zongmin Hu, Wenhao Wang, Zijian Zhang
doaj   +1 more source

Influence of coolant multi-jets on heat reduction of nose cone with blunt spike at hypersonic flow. [PDF]

Sci Rep, 2022
Ghanbari M, Maddah S, Alinejad J.
europepmc   +1 more source

Leading-edge bluntness effects on the hypersonic flow over the double wedge at multiple aft-wedge angles [PDF]

, 2023
Anurag Adityanarayan Ray, Ashoke De
openalex   +1 more source

Black-box optimization methods for hypersonic flow problems [PDF]

International Journal of Fluid Engineering
This review examines the application of black-box optimization methods to hypersonic flow problems, with a particular emphasis on scenarios where computational fluid dynamics (CFD) simulations function as opaque, nontransparent models.
Davood Hoseinzade, DiviaHarshaVardini R C, Ikhyun Kim   +2 more
doaj   +1 more source

Numerical study of lateral coolant jet on heat reduction over nose cone with double-aerodome at hypersonic flow. [PDF]

Sci Rep, 2022
Ghanbari M, Maddah S, Alinejad J.
europepmc   +1 more source

Study on the influence of the adiabatic index on the characteristics of a plane hypersonic input device of external compression

Авіаційно-космічна техніка та технологія
This study presents the main results of research on the assessment of the change in the influence of the adiabatic index on the total pressure conservation coefficient and the length of the direct compression jump in the supersonic part of the external ...
Artem Khorokhordin, Mykhailo Mitrakhovych   +1 more
doaj   +1 more source