Boundary-Layer Transition Detection in a Cryogenic Wind Tunnel Using Luminescent Paint

Boundary-Layer Transition Detection in a Cryogenic Wind Tunnel Using Luminescent Paint

A technique for boundary-layer transition detection in a cryogenic wind tunnel has been developed. This technique is based on the thermal quenching of luminescent molecules.

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of aircraft 1997-01, Vol.34 (1), p.34-42
Hauptverfasser: Asai, Keisuke, Kanda, Hiroshi, Kunimasu, Tetsuya, Liu, Tianshu, Sullivan, John P
Format: Artikel
Sprache:eng
Schlagworte:
Aerodynamics
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Instrumentation for fluid dynamics
Physics
Transition to turbulence
Turbulent flows, convection, and heat transfer
Wind tunnels
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:A technique for boundary-layer transition detection in a cryogenic wind tunnel has been developed. This technique is based on the thermal quenching of luminescent molecules.
ISSN:0021-8669
1533-3868
DOI:10.2514/2.2132