Parametric Study of Boundary-Layer Receptivity to Freestream Hot-Spot Perturbation Over a Blunt Compression Cone

doi 10.2514/6.2014-0774
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

Numerical Simulation of Graphite Ablation Induced Outgassing Effects on Hypersonic Boundary Layer Receptivity Over a Cone Frustum

2013English

Receptivity to Freestream Acoustic Noise in Hypersonic Flow Over a Generic Forebody

Journal of Spacecraft and Rockets
SpacePlanetary ScienceAerospace Engineering
2019English

Boundary Layer Stability Analysis for Stetson’s Mach 6 Blunt Cone Experiments

2016English

Hypersonic Boundary Layer Stability Over a Flared Cone in a Quiet Tunnel

1996English

Numerical Simulation of Leading Edge Receptivity of Stetson's Mach 8 Blunt Cone Stability Experiments

2003English

Analytical Solution of Laminar Boundary Layer Equations Over a Flat Plate by Homotopy Perturbation Method

International Journal of Applied Mathematical Research
2012English

Linear Stability Study of Hypersonic Boundary Layer Transition on Blunt Circular Cones

2009English

Homotopy Perturbation Method for MHD Boundary Layer Flow With Low Pressure Gradient Over a Flat Plate

Journal of Applied Fluid Mechanics
Mechanics of MaterialsCondensed Matter PhysicsMechanical Engineering
2014English

Laboratory Study on Oscillatory Boundary Layer Over a Ripple Model.

Doboku Gakkai Ronbunshu
1990English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy