๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Measurements of the response of a panel excited by shock boundary-layer interaction

โœ Scribed by L. Maestrello; T.L.J. Linden

Publisher
Elsevier Science
Year
1971
Tongue
English
Weight
538 KB
Volume
16
Category
Article
ISSN
0022-460X

No coin nor oath required. For personal study only.

๐Ÿ“œ SIMILAR VOLUMES

A WAVENUMBER APPROACH TO MODELLING THE R
A WAVENUMBER APPROACH TO MODELLING THE RESPONSE OF A RANDOMLY EXCITED PANEL, PART II: APPLICATION TO AIRCRAFT PANELS EXCITED BY A TURBULENT BOUNDARY LAYER
โœ C. MAURY; P. GARDONIO; S.J. ELLIOTT ๐Ÿ“‚ Article ๐Ÿ“… 2002 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 407 KB

Part I of this paper has shown the suitability of wavenumber}frequency approach in the calculation of the vibro-acoustic response of a thin ba%ed plate to a large class of random excitations. Part II describes the application of this formulation to the prediction of the vibration and the acoustic ra

A new numerical study of the shock/bound
A new numerical study of the shock/boundary-layer interaction
โœ Yiqing Shen; Ruquan Wang; Hongzhi Liao ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 177 KB ๐Ÿ‘ 2 views

This paper describes a new numerical study of the flat plate shock/boundary-layer interaction by using a weighted high-resolution, total variation diminishing (TVD) scheme. The key difference of this study from former studies is that new secondary vortices in the separated region have been found for

A Newton/upwind method and numerical stu
A Newton/upwind method and numerical study of shock wave/boundary layer interactions
โœ Meng-Sing Liou ๐Ÿ“‚ Article ๐Ÿ“… 1989 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 726 KB

The objective of the paper is twofold. First we describe an upwind/central differencing method for solving the steady Navier-Stokes equations. The symmetric line relaxation method is used to solve the resulting algebraic system to achieve high computational efficiency. The grid spacings used in the