Paper Title:
Design of S-Shaped Submerged Inlet
  Abstract

The influence of centerline and the cross-section variation to aerodynamic performance of the inlet was researched in a wider range. A new method of measuring the total pressure recovery coefficient and total pressure distortion coefficient of the inlet was proposed. Based on the loitering aircraft, a s-shaped inlet was designed to meet the needs of stable flight of loitering aircraft, whose total pressure recovery coefficient is 93.2% and total pressure distortion coefficient is 1.2%.

  Info
Periodical
Advanced Materials Research (Volumes 291-294)
Chapter
Modeling, Analysis and Simulation of Manufacturing Processes
Edited by
Yungang Li, Pengcheng Wang, Liqun Ai, Xiaoming Sang and Jinglong Bu
Pages
349-354
DOI
10.4028/www.scientific.net/AMR.291-294.349
Citation
G. L. He, X. L. Li, "Design of S-Shaped Submerged Inlet", Advanced Materials Research, Vols. 291-294, pp. 349-354, 2011
Online since
July 2011
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Price
$32.00
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