Thermal insulating layer for hot channel of hypersonic-velocity wind tunnel

The invention relates to a thermal insulating layer, and in particular relates to a thermal insulating layer for a hot channel of a hypersonic-velocity wind tunnel. The thermal insulating layer is in a cylindrical structure and comprises a cylinder body and two cylinder covers, wherein the cylinder...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HUANG JINGBO, XU RUIFENG, BU JUNHUI, MU DONGBO, SUN YONGTANG, CUI CHUN, JIA YINGSHENG, ZHAO XIAOYUN, SUN TAO, HUANG BINGXIU, SHI YUNJUN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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