Browse

다양한 출구조건이 적용된 초음속 흡입구 공력불안정성 수치적 연구
Numerical Analysis of Supersonic Inlet Buzz Characteristics Under Various Throttling Conditions

Cited 0 time in Web of Science Cited 0 time in Scopus
Authors
홍우람; 최요한; 김종암
Issue Date
2013-05
Publisher
한국전산유체공학회
Citation
한국전산유체공학회 2013년도 춘계학술대회 논문집, pp. 200-208
Keywords
공학전산유체역학(CFD)흡입구 버즈(Inlet Buzz)충격파 불안정성(Shock Instability)천이(Transition)입출구비(Throttling ratio, T.R)이력특성(Hysteretic Characteristic)
Abstract
The present study numerically investigates the flow instability around supersonic inlet, called inlet buzz. Though the flow conditions change linearly, behavior of inlet buzz alters hysteretically. In order to simulate the inlet buzz hysteretic character, computations are conducted with varying mass flow rate. The mass flow rate condition is controlled by an exit throttling plug which moves back and forth to change an exit area.
In this paper, a set of simulations with mass flow rate control are presented. This simulations focus on hysteretic buzz characteristics of supersonic inlet according to mass flow rate and the historic path of the mass flow rate change. Firstly, an inlet buzz case with decreasing mass flow rate is simulated. In this process, the inlet buzz characteristic changes from the first mode of a low frequency regime to the second mode of a high frequency regime. In the next, the effect of the increasing mass flow rate on the inlet buzz is examined. This case shows another kind of the buzz transition that the buzz frequency becomes higher in the third mode. The hysteretic inlet buzz has many similarities to the fundamentals of a pipe-type musical instrument such as self-excited feed-back mechanism and overblowing. Considering the similarities, the hysteretic characteristics of an inlet buzz is discussed in the instrumental acoustic point of view.
Language
Korean
URI
https://hdl.handle.net/10371/84887
Files in This Item:
Appears in Collections:
College of Engineering/Engineering Practice School (공과대학/대학원)Dept. of Mechanical Aerospace Engineering (기계항공공학부)Others_기계항공공학부
  • mendeley

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

Browse