SAE AIR6440 Icing Tunnel Tests for Thermal Ice Protection Systems
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时间:2024-04-24 02:29:42
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Product Code:SAE AIR6440
Title:Icing Tunnel Tests for Thermal Ice Protection Systems
Issuing Committee:Ac-9c Aircraft Icing Technology Committee
Scope: This document is intended to provide guidance for conducting icing tunnel tests for assessment and design of thermal anti-ice systems for wing, stabilizers and engine inlets (considering both hot air and electrical power as a heat source).
Rationale: This document is intended to provide guidance for conducting icing tunnel tests for assessment and design of thermal anti-ice systems for wing, stabilizers and engine inlets (considering both hot air and electrical power as a heat source).
Title:Icing Tunnel Tests for Thermal Ice Protection Systems
Issuing Committee:Ac-9c Aircraft Icing Technology Committee
Scope: This document is intended to provide guidance for conducting icing tunnel tests for assessment and design of thermal anti-ice systems for wing, stabilizers and engine inlets (considering both hot air and electrical power as a heat source).
Rationale: This document is intended to provide guidance for conducting icing tunnel tests for assessment and design of thermal anti-ice systems for wing, stabilizers and engine inlets (considering both hot air and electrical power as a heat source).
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