Quasi-equilibrium glide trajectory design of wave rider-based hypersonic vehicle

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The primary objective of this work is to carry out the 3D parametric geometry representations of hypersonic waveriders, and to calculate its aerodynamics by engineering experiential formula. Finally, an approach is proposed to determine a quasi-equilibrium glide trajectory with constraint on the stagnation point heat transfer rate. The benefit of solving this problem is that the angle of attack is the only control to be determined.

Original languageEnglish
Title of host publicationICMET 2010 - 2010 International Conference on Mechanical and Electrical Technology, Proceedings
Pages408-412
Number of pages5
DOIs
StatePublished - 2010
Event2010 International Conference on Mechanical and Electrical Technology, ICMET 2010 - Singapore, Singapore
Duration: 10 Sep 201012 Sep 2010

Publication series

NameICMET 2010 - 2010 International Conference on Mechanical and Electrical Technology, Proceedings

Conference

Conference2010 International Conference on Mechanical and Electrical Technology, ICMET 2010
Country/TerritorySingapore
CitySingapore
Period10/09/1012/09/10

Keywords

  • Hypersonic
  • Quasi-equilibrium glide
  • Waverider

Fingerprint

Dive into the research topics of 'Quasi-equilibrium glide trajectory design of wave rider-based hypersonic vehicle'. Together they form a unique fingerprint.

Cite this