1989•Medical Entomology and ZoologyRequires access

Defining the hypersonic environment

John J. Bertin, R. Glowinski, Jacques Périaux

Abstract

Aerothermodynamic Phenomena and the Design of Atmospheric Hypersonic Airplanes.- Concepts of Hypersonic Aircraft.- Hypersonic Wind Tunnel Testing.- Wind-Tunnel Based Definition of the AFE Aerothermodynamic Environment.- High-Enthalpy Testing in Hypersonic Shock Tunnels.- Low Density Facilities.- Hypersonic Boundary-Layer Transition.- Some Viscous Interactions Affecting the Design of Hypersonic Intakes and Nozzles.- Permissions.

About this research paper

What this paper is about

Why it matters

OpenAlex reports 4 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Key concepts: Hypersonic speed, Hypersonic flight, Expansion tunnel, Hypersonic wind tunnel, Aerospace engineering, Shock (circulatory), Wind tunnel, Nozzle