Access the full text.
Sign up today, get DeepDyve free for 14 days.
Loading next page...
/lp/springer-journals/experimental-study-of-the-influence-of-small-angles-of-attack-and-cone-ai0TapLRmK
References (25)
-
M. Hites (1998)
Problems in high speed flow prediction relevant to control, 2nd AIAA Theoretical Fluid Mechanics Meeting -
A. Fedorov, V. Soudakov, I. Egorov, A. Sidorenko, Y. Gromyko, D. Bountin, P. Polivanov, A. Maslov (2015)
High-Speed Boundary-Layer Stability on a Cone with Localized Wall Heating or CoolingAIAA Journal, 53
-
P. Paredes, Meelan Choudhari, Fei Li (2017)
Stabilization of Hypersonic Boundary Layers by Linear and Nonlinear Optimal Perturbations -
E. Marineau, C. Moraru, Daniel Lewis, J. Norris, J. Lafferty, H. Johnson (2015)
Investigation of mach 10 boundary layer stability of sharp cones at angle-of-attack, part 1: Experiments -
A. Rasheed, H. Hornung, A. Fedorov, N. Malmuth (2002)
Experiments on passive hypervelocity boundary-layer control using an ultrasonically absorptive surfaceAIAA Journal, 40
-
A. Fedorov, A. Shiplyuk, A. Maslov, E. Burov, N. Malmuth (2003)
Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coatingJournal of Fluid Mechanics, 479
-
K. Stetson, E. Thompson, J. Donaldson, L. Siler (1985)
Laminar boundary layer stability experiments on a cone at Mach 8. III - Sharp cone at angle of attack -
A. Fedorov, N. Malmuth, A. Rasheed, H. Hornung (2001)
Stabilization of Hypersonic Boundary Layers by Porous CoatingsAIAA Journal, 39
-
K. Hannemann (2013)
Hypersonic boundary-layer stabilization by means of ultrasonically absorptive carbon-carbon material, Part 1: Experimental Results, in: 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Aerospace Sciences Meetings -
I. Egorov, V. Sudakov, A. Fedorov (2006)
Numerical modeling of the stabilization of a supersonic flat-plate boundary layer by a porous coatingFluid Dynamics, 41
-
Xiaowen Wang, X. Zhong (2012)
The stabilization of a hypersonic boundary layer using local sections of porous coatingPhysics of Fluids, 24
-
A. Fedorov, V. Soudakov, Ivett Levya (2014)
Stability Analysis of High-Speed Boundary-Layer Flow with Gas Injection -
P.A. Polivanov Yu.V. Gromyko (2013)
An experimental study of the natural noise in the Transit-M hypersonic wind tunnelThermophysics and Aeromechanics, 20
-
M.M. Choudhari (2017)
Stabilization of hypersonic boundary layers by linear and nonlinear optimal perturbations, in: 47th AIAA Fluid Dynamics Conference -
D. Bountin, A. Maslov (2017)
Analysis of the development of perturbations in a hypersonic boundary layer behind a wavy surfaceTechnical Physics Letters, 43
-
S. Lukashevich, S. Morozov, A. Shiplyuk (2016)
Experimental study of the effect of a passive porous coating on disturbances in a hypersonic boundary layer 2. Effect of the porous coating locationJournal of Applied Mechanics and Technical Physics, 57
-
S. Lukashevich, S. Morozov, A. Shiplyuk (2018)
Experimental investigation of the effect of a passive porous coating on a hypersonic boundary layer stability on a sharp cone at an angle of attack -
V. Wartemann, T. Eggers, T. Giese, A. Wagner, K. Hannemann (2013)
Hypersonic boundary-layer stabilization by means of ultrasonically absorptive carbon-carbon material Part 2: Computational Analysis -
(2013)
An experimental study of the natural noise in the Transit-M hypersonic wind tunnel, Thermophysics and Aeromechanics -
A. Fedorov (2011)
Transition and Stability of High-Speed Boundary LayersAnnual Review of Fluid Mechanics, 43
-
J.F. Lafferty (2015)
Investigation of Mach 10 boundary layer stability of sharp cones at angle-of-attack, Part 1, Experiments, in: 53rd AIAA Aerospace Sci. Meeting -
N. Malmuth, A. Fedorov, V. Shalaev, J. Cole, M. Hites, D. Williams, A. Khokhlov (1998)
Problems in high speed flow prediction relevant to control -
J.C. Donaldson (1985)
Laminar boundary layer stability experiments on a cone at Mach 8. Part III: sharp cone at angle of attack, in: 23rd Aerospace Sci. Meeting -
S. Lukashevich, S. Morozov, A. Shiplyuk (2013)
Experimental study of the effect of a passive porous coating on disturbances in a hypersonic boundary layer. 1. Effect of the porous coating lengthJournal of Applied Mechanics and Technical Physics, 54
-
S. Lukashevich, S. Morozov, A. Shiplyuk (2012)
Experimental study of the influence of parameters of a passive porous coating on the development of disturbances in a hypersonic boundary layerTechnical Physics Letters, 38
- Publisher
- Springer Journals
- Copyright
- 2018 S.O. Morozov, S.V. Lukashevich, V.G. Soudakov, and A.N. Shiplyuk
- ISSN
- 0869-8643
- eISSN
- 1531-8699
- DOI
- 10.1134/S086986431806001X
- Publisher site
- See Article on Publisher Site
Abstract
Abstract The present work was devoted to an experimental study of small angles of attack and cone nose bluntness on the efficiency of stabilization of high-frequency disturbances in hypersonic boundary layer with a passive porous coating. The experiments were carried out on a cone with an apex half-angle 7° and nose bluntness radii R = 0.03, 0.5 and 1 mm installed under angles of attack α = 0–1° at the freestream Mach number M∞ = 5.8. High-frequency pressure fluctuations on the sides of the cone with the solid and porous surfaces were measured. It is shown that at all angles of attack and cone bluntness, the passive porous coating permits an efficient suppression of disturbances in hypersonic boundary layer both on the windward and leeward sides of the cone.
Journal
Thermophysics and Aeromechanics – Springer Journals
Published: Nov 1, 2018