The Turn Rate Indicator - Its Interpretation as Affected by Installation and True Airspeed

710380

02/01/1971

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
The effects of mounting an airplane turn rate gyro at various angles relative to the roll axis of the vehicle have been investigated in flight. The range of suitable mounting angles varies not only with the amount of roll rate sensing desired for lead information, but also with the true airspeed of the airplane. Tilting the gyro in a face-up direction, as occasionally happens on a slightly inclined instrument panel, might have disastrous results if the instrument is relied on for recovery from an unusual attitude. Turn rate information is of very limited value on airplanes having high subsonic cruise speed.
Meta TagsDetails
DOI
https://doi.org/10.4271/710380
Pages
8
Citation
Stinnett, G., Jackson, C., and Talbot, P., "The Turn Rate Indicator - Its Interpretation as Affected by Installation and True Airspeed," SAE Technical Paper 710380, 1971, https://doi.org/10.4271/710380.
Additional Details
Publisher
Published
Feb 1, 1971
Product Code
710380
Content Type
Technical Paper
Language
English