Simulation Model Development for Icing Effects Flight Training Bihrle Applied Research, Incorporated

Format:

Conference/Event

Author/Creator:

Barnhart, Billy P., author.

Conference Name:

General Aviation Technology Conference & Exhibition (2002-04-16 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2002

Summary:

A high-fidelity simulation model for icing effects flight training was developed from wind tunnel data for the DeHavilland DHC-6 Twin Otter aircraft. First, a flight model of the un-iced airplane was developed and then modifications were generated to model the icing conditions. The models were validated against data records from the NASA Twin Otter Icing Research flight test program with only minimal refinements being required. The goals of this program were to demonstrate the effectiveness of such a simulator for training pilots to recognize and recover from icing situations and to establish a process for modeling icing effects to be used for future training devices

Notes:

Vendor supplied data

Publisher Number:

2002-01-1527

Access Restriction:

Restricted for use by site license