liu.seSearch for publications in DiVA
Change search
ReferencesLink to record
Permanent link

Direct link
One-Dimensional Human Thermoregulatory Model of Fighter Pilots in Cockpit Environments
Linköping University, Department of Management and Engineering, Applied Thermodynamics and Fluid Mechanics.
2015 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

During flight missions, fighter pilots are in general exposed to vast amounts of stress including mild hypoxia, vibrations, high accelerations, and thermal discomfort. It is interesting to predict potential risks with a certain mission or flight case due to these stresses to increase safety for fighter pilots. The most predominant risk is typically thermal discomfort which can lead to serious health concerns. Extensive exposure to high or low temperature in combination with a demanding work situation weakens the physical and mental state of the pilot and can eventually lead to life-threatening conditions. One method to estimate the physical and mental state of a person is to measure the body core temperature. The body core temperature cannot be measured continuously during flight and needs to be estimated by using for instance a human thermoregulatory model.

In this study, a model of the human thermoregulatory system and the cockpit environment is developed. Current thermoregulatory models are not customized for fighter pilots but a model developed by Fiala et al. in 2001, which has previously shown good performance in both cold and warm environments as well as for various activation levels for the studied person, is used as a theoretical foundation. Clothing layers are implemented in the model corresponding to clothes used by pilots in the Swedish air force flying the fighter aircraft Gripen E in warm outside conditions. Cooling garments and air conditioning systems as well as avionics, canopy, and cockpit air are included in the model to get a realistic description of the cockpit environment. Input to the model is a flight case containing data with altitude and velocity of the fighter during a mission.

human heat transfer; body temperature regulation; physiological model;cooling garment; cockpit modeling

Place, publisher, year, edition, pages
2015. , 86 p.
Keyword [en]
human heat transfer; body temperature regulation; physiological model; cooling garment; cockpit modeling
National Category
Mechanical Engineering
URN: urn:nbn:se:liu:diva-125528ISRN: LIU-IEI-TEK-A–15/02366–SEOAI: diva2:906798
External cooperation
Subject / course
Applied Thermodynamics and Fluid Mechanics
2015-08-21, Linköping, 10:15 (Swedish)
Available from: 2016-02-25 Created: 2016-02-25 Last updated: 2016-02-25Bibliographically approved

Open Access in DiVA

fulltext(2589 kB)56 downloads
File information
File name FULLTEXT01.pdfFile size 2589 kBChecksum SHA-512
Type fulltextMimetype application/pdf

By organisation
Applied Thermodynamics and Fluid Mechanics
Mechanical Engineering

Search outside of DiVA

GoogleGoogle Scholar
Total: 56 downloads
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

Total: 2564 hits
ReferencesLink to record
Permanent link

Direct link