Amanote Research

Amanote Research

    RegisterSign In

Conceptual Design for an Electron-Beam Heated Hypersonic Wind Tunnel

doi 10.2172/522724
Full Text
Open PDF
Abstract

Available in full text

Date

July 1, 1997

Authors
R.J. LipinskiR.P. Kensek
Publisher

Office of Scientific and Technical Information (OSTI)


Related search

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

Design and Optimization of Directly Heated LaB6 Cathode Assemblies for Electron‐beam Instruments

Journal of Vacuum Science and Technology
Engineering
1978English

Development of Pulsed Arc Heater for Small Hypersonic High-Enthalpy Wind Tunnel

Journal of Spacecraft and Rockets
SpacePlanetary ScienceAerospace Engineering
1999English

Boundary-Layer Transition Experiments in a Hypersonic Quiet Wind Tunnel

2013English

Electron Beam Heated Evaporation Using a Porous Material.

SHINKU
1997English

A Hybrid Airfoil Design Method for Icing Wind Tunnel Tests

2013English

The Aerospace Hypersonic Shock Tunnel

1963English

Investigation of Flow Field in a Typical Hypersonic Wind Tunnel Over a Standard Mode

Journal of Applied Fluid Mechanics
Mechanics of MaterialsCondensed Matter PhysicsMechanical Engineering
2013English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy