✦ LIBER ✦

Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height Roughness

✍ Scribed by Duan, Le; Wang, Xiaowen; Zhong, Xiaolin

Book ID: 120059760
Publisher: American Institute of Aeronautics and Astronautics
Year: 2013
Tongue: English
Weight: 823 KB
Volume: 51
Category: Article
ISSN: 0001-1452
DOI: 10.2514/1.J051643

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Disturbances of a three-dimensional boun

Disturbances of a three-dimensional boundary layer generated by surface roughness

✍ S. V. Manuilovich 📂 Article 📅 1990 🏛 Springer 🌐 English ⚖ 568 KB

Nonlinear waves and stabilization of two

Nonlinear waves and stabilization of two-dimensional instability in a boundary layer

✍ V. P. Reutov 📂 Article 📅 1986 🏛 SP MAIK Nauka/Interperiodica 🌐 English ⚖ 723 KB

Effects of roughness blocks on atmospher

Effects of roughness blocks on atmospheric boundary layer flow over a two-dimensional low hill with/without sudden roughness change

✍ Shuyang Cao; Tetsuro Tamura 📂 Article 📅 2007 🏛 Elsevier Science 🌐 English ⚖ 376 KB

The perturbation of a turbulent boundary

The perturbation of a turbulent boundary layer by a two-dimensional hill

✍ Erick de Moraes Franklin… 📂 Article 📅 2013 🏛 SciELO 🌐 English ⚖ 767 KB

Numerical simulation of a three-dimensio

Numerical simulation of a three-dimensional shock wave-turbulent boundary layer interaction generated by a sharp fin at Mach 4

✍ D.D. Knight 📂 Article 📅 1990 🏛 Elsevier Science ⚖ 630 KB

The three-dimensional inviscid-viscous interaction generated by the intersection of an oblique shock with a turbulent boundary layer is examined theoretically. An incoming Mach 4 equilibrium turbulent boundary layer at Reynolds number Re~ = 2 × 105 interacts with an oblique shock formed by a 16 ° sh

Sound produced by turbulent boundary lay

Sound produced by turbulent boundary layer flow over a finite region of wall roughness, and over a forward facing step

✍ M.S. Howe 📂 Article 📅 1989 🏛 Elsevier Science 🌐 English ⚖ 788 KB

An analysis is made of the sound produced during low Mach number turbulent flow over a roughened section of a nominally plane, rigid wall. The wall is roughened over a finite distance in the mean flow direction, and the roughness elements are modeled by a random distribution of hemispherical bosses.