Flow-Field Measurements in the Windward Surface Shock Layer of Space Shuttle Orbiter Configurations at Mach Number 8

doi 10.21236/ada012875
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Defense Technical Information Center

Related search

The Effect of Mach Number on Unstable Disturbances in Shock/Boundary-Layer Interactions

Physics of Fluids
Mechanics of MaterialsCondensed Matter PhysicsMechanical EngineeringFluid FlowTransfer ProcessesComputational Mechanics
2007English

Dependence on Shock Mach Number of the Shock-Vortex Ring Interaction.

Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Condensed Matter PhysicsMechanical Engineering
2000English

Nonthermal Electrons at High Mach Number Shocks: Electron Shock Surfing Acceleration

Astrophysical Journal
AstrophysicsAstronomyPlanetary ScienceSpace
2002English

Transient Growth in Oblique Shock Wave/Laminar Boundary Layer Interactions at Mach 5.92

2018English

POLAR Code Calculations of the Shuttle Orbiter Plasma Wake and Direct Comparisons With Spacelab II Measurements.

1986English

Active Control of Wall Pressure Flow Field at Low Supersonic Mach Numbers

IOSR Journal of Mechanical and Civil Engineering
2016English

Transition to Turbulence in Shock-Driven Mixing: A Mach Number Study

Journal of Fluid Mechanics
Mechanics of MaterialsCondensed Matter PhysicsMechanical Engineering
2011English

Numerical Analysis of Flow Over NACA0012 at Fixed Mach Number Using Computational Fluid Dynamics

International Journal of Mechanical and Production Engineering Research and Development
Transfer ProcessesFluid FlowMechanical EngineeringAerospace Engineering
2017English

Mean Flow and Turbulence Measurements in the Near Field of a Fighter Aircraft Wing-Tip Vortex at High Reynolds Number and Transonic Flow Conditions

ESAIM: Proceedings
1999English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy