A NUMERICAL STUDY FOR SMALL AMPLITUDE TS WAVES IN A SUPERSONIC BOUNDARY LAYER

被引：0

作者：

袁湘江

周恒

机构：

来源：

Applied Mathematics and Mechanics(English Edition) | 2000年 / 12期

关键词：

direct numerical simulation; shocklet; compressible boundary layeD;

D O I：

暂无

中图分类号：

V211.1 [理论空气动力学];

学科分类号：

摘要：

The propagation of the disturbance waves in a boundary layer at Mach number= 4 5 is studied by direct numerical simulation (DNS), using NND scheme, and different amplitudes A=0 01, 0 001, 0 000 1 of the disturbance have been assumed. The numerical result shows that there might be shocklets induced in the boundary layer, even when the amplitude of disturbance wave is still small.

引用

页码：1341 / 1344

页数：4

共 50 条

[1] A numerical study for small amplitude T-S waves in a supersonic boundary layer
Yuan, XJ
Zhou, H
LAMINAR-TURBULENT TRANSITION, 2000, : 433 - 436
[2] A numerical study for small amplitude T-S waves in a supersonic boundary layer
Yuan, XJ
Zhou, H
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2000, 21 (12) : 1341 - 1344
[3] THE RESPONSE OF A LAMINAR BOUNDARY-LAYER IN SUPERSONIC-FLOW TO SMALL-AMPLITUDE PROGRESSIVE WAVES
DUCK, PW
JOURNAL OF FLUID MECHANICS, 1990, 219 : 423 - 448
[4] NUMERICAL STUDY OF SUPERSONIC TURBULENT BOUNDARY-LAYER OVER A SMALL PROTUBERANCE
POLAK, A
AIAA JOURNAL, 1974, 12 (10) : 1409 - 1411
[5] Numerical investigations of small-amplitude disturbances in a laminar boundary layer with impinging shock waves
Pagella, A
Rist, U
Wagner, S
NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS III, 2002, 77 : 153 - 160
[6] Numerical Simulation of the Supersonic Boundary Layer Interaction with Arbitrary Oriented Acoustic Waves
Semenov, A. N.
Gaponov, S. A.
PROCEEDINGS OF THE XXV CONFERENCE ON HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2017), 2017, 1893
[7] Selective enhancement of oblique waves caused by finite amplitude second mode in supersonic boundary layer
Zhang, Cunbo
Luo, Jisheng
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2017, 38 (08) : 1109 - 1126
[8] Selective enhancement of oblique waves caused by finite amplitude second mode in supersonic boundary layer
Cunbo ZHANG
Jisheng LUO
Applied Mathematics and Mechanics(English Edition), 2017, 38 (08) : 1109 - 1126
[9] Selective enhancement of oblique waves caused by finite amplitude second mode in supersonic boundary layer
Cunbo Zhang
Jisheng Luo
Applied Mathematics and Mechanics, 2017, 38 : 1109 - 1126
[10] Nonlinear development of waves in the supersonic boundary layer
Gaponov, S.A.
Kosinov, A.D.
Maslennikova, I.I.
Semionov, N.V
Shevel'kov, S.G.
1994,

← 1 2 3 4 5 →