Circular-arc jet flaps at hypersonic speeds [PDF]
Peer Reviewed ; http://deepblue.lib.umich.edu/bitstream/2027.42/76220/1/AIAA-1970-553-639 ...
openaire +1 more source
Suboptimal Midcourse Guidance with Terminal-Angle Constraint for Hypersonic Target Interception
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
Assessment of Solution of the Boundary Layer Equations and Approximate Relations for Aeroheating of Axisymmetric Reentry Vehicles [PDF]
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
Viscous equilibrium analysis of heat transfer on blunted cone at hypersonic flow
High speed flow requires consideration of some complex phenomena such as chemical reactions. In fact, as flow velocity increase, high temperature of hypersonic velocity excites molecules to react and causes dissociation and ionization.
F. Pish +3 more
doaj +1 more source
RBFNN-Based Anti-Input Saturation Control for Hypersonic Vehicles
In hypersonic flight control, characterized by challenges posed by input saturation, model parameter uncertainties, and external disturbances, this paper introduces a pioneering anti-input saturation control method based on RBFNN adaptivity.
Bangchu Zhang +4 more
doaj +1 more source
Modeling and control of hypersonic vehicle dynamic under centroid shift
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
NUMERICAL MODELING AND DYNAMIC SIMULATIONS OF NONLINEAR AEROTHERMOELASTIC OF A DOUBLE-WEDGE LIFTING SURFACE [PDF]
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
Optimization and Analysis on Trajectory with Multiple Constraints for Hypersonic Air-vehicle
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
High-Speed PLIF Imaging of Hypersonic Transition over Discrete Cylindrical Roughness [PDF]
Paul M. Danehy +10 more
openalex +1 more source
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
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