NONLINERA COUPLING ANALYSIS FOR HYPERSONIC FLIGHT VEHICLE

Abstract

 Based on 3D figuration, the nonlinear coupling between the airframe and scramjet for hypersonic vehicle is investigated in this paper. Firstly, a free-free beam structure elastic model is utilized taking into account of varying cross-section moment of inertia and uneven mass, and 3D elastic deformations are introduced. Then, the coupling dynamic equation is established and the coupling characteristics among the 3D aerodynamics, structure elastic deformation and propulsion are analyzed. The solution of the thrust force and its relation with the elastic deformation are presented and analyzed qualitatively and quantitatively. The results show that the elastic deformation of the structure affects the thrust force of scramjet significantly which provide very important information for the operation of scramjet and control of hypersonic vehicle

Authors and Affiliations

Erlong Su* ,

Keywords

Related Articles

EFFECTIVE DATA MINING USING NEURAL NETWORKS

Classification is one of the data mining problems receiving great attention recently in the database community. This paper presents an approach to discover symbolic classification rules using neural networks. Neural net...

 Analysis of Effectiveness of ALERT Protocol against Wormhole Attack in MANETs

 Routing in MANETs is one of the challenging issues because it dynamically changes their topology over the time and hence requires an efficient routing protocol to communicate among the mobile nodes. There are seve...

 PERFORMANCE EVALUATE OF PARTIALLY DEPLETED AND FULLY DEPLETED SOI MOSFET AT 32 NM TECHNOLOGY

 this this paper presents an performance evaluate of partially depleted soi (pdsoi) mosfet and fully depleted soi (fdsoi) mosfet at 32 nm technology. Silicon on insulator (SOI) technology refers for use of a layere...

 INFLUENCE OF WELDING SPEED AND GROOVE ANGLE ON STRENGTH OF V-GROOVE BUTT WELD JOINT USING TIG WELDING

 Welding is the metal joining process in which two or more metal having same material or different can be joined by heating to a plastic state .It is mostly used for joining metals in process industry, in fabricati...

 IMPACT OF NATURE OF LOAD ON FACT DEVICES (UPFC) BY ANALYSING THE POWER FACTOR OF LOAD BUS

 In today’s era of technology, the power distribution took revolutionary changes. Many researches have been done to improve power quality and many are under process. In spite of some one more factor pull-up that po...

Download PDF file
  • EP ID EP143169
  • DOI -
  • Views 73
  • Downloads 0

How To Cite

Erlong Su*, (0).  NONLINERA COUPLING ANALYSIS FOR HYPERSONIC FLIGHT VEHICLE. International Journal of Engineering Sciences & Research Technology, 4(9), 236-245. https://europub.co.uk/articles/-A-143169