Oxide‐Based Ceramic Matrix Composites for High‐Temperature Environments: A Review
Advanced Engineering Materials, Volume 27, Issue 7, April 2025.This review examines oxide‐based ceramic matrix composites, focusing on their processing, composition, and mechanical properties for high‐temperature applications. Key topics include oxidation resistance, failure mechanisms, and corrosion behavior, with insights into their potential use in aerospace, nuclear power, and other high‐performance industries.
Karthikeyan Ramachandran +2 more
wiley +1 more source
Eulerian discrete kinetic framework in comoving reference frame for hypersonic flows
Journal of Fluid MechanicsFlow physics vary in different regimes across the full Mach number range, with our knowledge being particularly poor about the hypersonic regime. An Eulerian realization of the particles on demand method, a kinetic model formulated in the comoving ...
Y. Ji +4 more
semanticscholar +1 more source
Suboptimal Midcourse Guidance with Terminal-Angle Constraint for Hypersonic Target Interception
International Journal of Aerospace Engineering, 2019 For the problem of hypersonic target interception, a novel midcourse guidance method with terminal-angle constraint is proposed. Referring to the air-breathing and the boost-gliding hypersonic targets, flight characteristics and difficulties of ...
Shizheng Wan +3 more
doaj +1 more source
Optimization and Analysis on Trajectory with Multiple Constraints for Hypersonic Air-vehicle
MATEC Web of Conferences, 2015 The trajectory optimization technology is one of the key technologies for hypersonic air-vehicle. There are multiple constraints in the process of hypersonic flight, such as uncertainty of flight environment, thermal current, dynamic pressure and ...
Wei Changzhu +3 more
doaj +1 more source
Assessment of Solution of the Boundary Layer Equations and Approximate Relations for Aeroheating of Axisymmetric Reentry Vehicles [PDF]
فصلنامه علوم و فناوری فضایی, 2013 When a solver is used for analyzing the hypersonic reentry vehicles, high speed and accuracy of the solver results are the basic parameters in the design process.
R. Kamali –Moghadam +4 more
doaj
Shock-Wave Effects on the Laminar Skin Friction of an Insulated Flat Plate at Hypersonic Speeds [PDF]
, 1953 Ting-Yi Li, H. T. Nagamatsu
openalex +1 more source
NUMERICAL MODELING AND DYNAMIC SIMULATIONS OF NONLINEAR AEROTHERMOELASTIC OF A DOUBLE-WEDGE LIFTING SURFACE [PDF]
Journal of Engineering Science and Technology, 2008 The design of the re-entry space vehicles and high-speed aircrafts requires special attention to the nonlinear thermoelastic and aerodynamic instabilities of their structural components.
ARIF A. EBRAHEEM AL-QASSAR
doaj
Modeling and control of hypersonic vehicle dynamic under centroid shift
Advances in Mechanical Engineering, 2018 Due to the huge flight scale and the fast speed of hypersonic vehicle, the system must be of strong nonlinearity, coupling, and fast time variability, which give rise to the huge challenge for the design of controller.
Yizhen Meng, Bin Jiang, Ruiyun Qi
doaj +1 more source
Modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speeds. [PDF]
, 1966 E. Carson Yates
openalex +1 more source
International Journal of Aerospace Engineering, 2019 In order to overcome the drag at hypersonic speed, hypersonic flight vehicles require a high level of integration between the airframe and the propulsion system.
Sergio Nicolas Pachón Laitón +4 more
doaj +1 more source