Please use this identifier to cite or link to this item:
Title: Development of a smart nozzle
Authors: Huang, Xiaoyang.
Keywords: DRNTU::Engineering::Manufacturing
Issue Date: 1999
Abstract: This work is currently at a very preliminary stage. The performance test of the nozzle was limited at low Mach numbers and low frequencies, due to several facts, including the low speed of the control hardware. Further studies will obviously be necessary to improve the control system and to extend the test to high speed jet flows, e.g., supersonic jets, where screech tones may occur.
Rights: Nanyang Technological University
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:MAE Research Reports (Staff & Graduate Students)

Files in This Item:
File Description SizeFormat 
  Restricted Access
7.67 MBAdobe PDFView/Open

Google ScholarTM


Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.