Amanote Research

Amanote Research

    RegisterSign In

The Aerospace Hypersonic Shock Tunnel

doi 10.21236/ad0403052
Full Text
Open PDF
Abstract

Available in full text

Date

February 21, 1963

Authors
Robert L. Varwig
Publisher

Defense Technical Information Center


Related search

Pressure-Sensitive Paint Measurements of Hypersonic Flow in Shock Tunnel

Journal of the Japan Society for Aeronautical and Space Sciences
2003English

Radiatively Driven Hypersonic Wind Tunnel

AIAA Journal
Aerospace Engineering
1995English

Humidity Management for a Hypersonic Wind Tunnel

Journal of the Japan Society for Aeronautical and Space Sciences
2007English

Performance Tests of the Kyoto University Hypersonic Gun Tunnel.

The Journal of the Japan Society of Aeronautical Engineering
1963English

Computations of Axisymmetric Flows in Hypersonic Shock Tubes

Journal of Thermophysics and Heat Transfer
Condensed Matter PhysicsMechanical EngineeringSpaceFluid FlowPlanetary ScienceTransfer ProcessesAerospace Engineering
1996English

Hypersonic Transition Research in the Boeing/Afosr Mach-6 Quiet Tunnel

2003English

Boundary-Layer Transition Experiments in a Hypersonic Quiet Wind Tunnel

2013English

Conceptual Design for an Electron-Beam Heated Hypersonic Wind Tunnel

1997English

Character of Hypersonic Shock Tunnels With Real Gas Effects

The Journal of the Japan Society of Aeronautical Engineering
1968English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy