Specialists in Aircraft
   In-Flight Icing

IHB – Icing Heat Balance

Introduction

The IHB (Icing Heat Balance) code performs a steady-state thermal analysis on a heated, thin strip, structure in two-dimensions. The code performs a ‘Messinger’ type heat balance on the breeze surface, to calculate the local freezing fraction and surface temperature. The local ice growth rate (mm/min) is then calculated from the local freezing fraction and the cloud water droplet impact rate. The ice growth rates are then extrapolated to the required time in icing and an ice profile is produced by growing the ice normal to the body surface. External heat (in Watts/m2) may be specified at various chord wise locations to simulate the heat input from an ice protection system, and the code will calculate whether ice still grows, the surface runs wet, or the water is fully evaporated. The code requires a user input file which specifies the distribution of water catch, heat transfer coefficient and surface pressure ratio or pressure coefficient. This information is usually provided by the TAC2 code.

Technical

The code has three primary modes of operation (run-type options). These are specified by the user in the input file using the parameter RTYPE. The currently accepted values are 0, 1, -1 or 2. The following options are thus currently available;

Example ice shape, NATO RTO Case 18

Example ice shape, NATO RTO Case 18

Example ice shape, NATO RTO Case 9

Example ice shape, NATO RTO Case 9

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