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Aerodynamic coefficients models of hypersonic vehicle based on aero database

  • Guangren Duan*
  • , Yong Sun
  • , Maorui Zhang
  • , Ze Zhang
  • , Xiangyu Gao
  • *Corresponding author for this work
  • Harbin Institute of Technology

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

Abstract

The aerodynamic Coefficients models play an essential part in the simulation and the analysis of the hypersonic vehicle, especially in the trajectory planning. This paper builds the aerodynamic coefficients models by the nonlinear least square method based on the CAV aero database. The lift and drag coefficients models can be expressed with the polynomial and the exponential function. The parameters of the model have been gotten and the mean of relative error is less than 5.10%. So the models fit the aero characteristic well and can be used in practical design and simulation as a reference.

Original languageEnglish
Title of host publicationProceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010
Pages1001-1004
Number of pages4
DOIs
StatePublished - 2010
Event1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010 - Harbin, China
Duration: 17 Sep 201019 Sep 2010

Publication series

NameProceedings - 2010 1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010

Conference

Conference1st International Conference on Pervasive Computing, Signal Processing and Applications, PCSPA 2010
Country/TerritoryChina
CityHarbin
Period17/09/1019/09/10

Keywords

  • Aerodynamic coefficients
  • CAV
  • Hypersonic vehicle
  • Nonlinear least square

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