Numerical simulation of loitering aircraft aerodynamics in low speed flight

Guanglin He*, Xiaolin Li

*Corresponding author for this work

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

Abstract

Aerodynamic design rules of unconventional layout loitering aircraft against the issue of stall in low speed flight were proposed in this paper. Using the SST k-ω two equations turbulence model, the stalling characteristics of the loitering aircraft were studied. Based on the low speed flow field of the loitering aircraft without the deflexion of the helm, aerodynamic parameters such as lift, drag, pitching moment and yawing moment in different workings were calculated. Analysis of the results shows that the loitering aircraft designed has good stalling capability whose critical angle of attack is 18 degrees. The loitering aircraft has good longitudinal and lateral stability under different angle of attack.

Original languageEnglish
Title of host publicationAdvanced Research on Industry, Information System and Material Engineering
Pages139-143
Number of pages5
DOIs
Publication statusPublished - 2011
Externally publishedYes
Event2011 International Conference on Industry, Information System and Material Engineering, IISME2011 - Guangzhou, China
Duration: 16 Apr 201117 Apr 2011

Publication series

NameAdvanced Materials Research
Volume204-210
ISSN (Print)1022-6680

Conference

Conference2011 International Conference on Industry, Information System and Material Engineering, IISME2011
Country/TerritoryChina
CityGuangzhou
Period16/04/1117/04/11

Keywords

  • Loitering aircraft
  • Numerical simulation
  • Stalling capability

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