AIR-TEMPERATURE REGULATION EFFECTS ON FUEL ECONOMY

1921 ◽  
Author(s):  
Reuben E Fielder
1982 ◽  
Vol 60 (4) ◽  
pp. 491-494 ◽  
Author(s):  
Jacques Larochelle ◽  
Jeffrey Delson ◽  
Knut Schmidt-Nielsen

Metabolic rate, body temperature, and heat dissipating mechanisms of the Black Vulture were studied under laboratory conditions. The metabolic rate (6.5 W) was close to the predicted one. The body temperature showed considerable variations with air temperature, ranging from 37.7 °C at 15 °C to 42.9 °C at 45 °C. The area of featherless skin on the head and neck changed with the body temperature, thus indicating a role in heat dissipation, and we conclude that these featherless skin areas can be adjusted according to the need for temperature regulation.


1984 ◽  
Vol 62 (5) ◽  
pp. 808-813 ◽  
Author(s):  
Roger M. Evans

Body temperatures (Tb) of young white pelicans (Pelecanus erythrorhynchos) were measured in a breeding colony and in the laboratory. The newly hatched naked young were essentially poikilothermic, but an average air temperature (Ta) of over 31 °C was maintained in the colony by parental brooding which usually kept the nest temperature at 26–28 °C. A marked increased in thermogenesis, shivering, and natal down growth occurred by about 13–14 days of age. By 16–18 days, Tb measured after 2 h at 10, 20, and 30 °C in the laboratory ranged from 35 to 40 °C, and was similar to older downy young monitored in the colony. Young were able to gular flutter on the day of hatching, but this was not seen in the colony until 11 ± 2 days of age. Gular fluttering was more common in young exposed to full sun than under cloud. In the sun, gular fluttering began at about 19.5 °C, and increased in frequency with air temperature. Onset occurred at Tb of about 39–40 °C. The onset of functional temperature regulation by about 15–18 days of age correlates with the time that both parents begin to forage overnight, leaving their young unattended.


Author(s):  
W. T. Donlon ◽  
J. E. Allison ◽  
S. Shinozaki

Light weight materials which possess high strength and durability are being utilized by the automotive industry to increase fuel economy. Rapidly solidified (RS) Al alloys are currently being extensively studied for this purpose. In this investigation the microstructure of an extruded Al-8Fe-2Mo alloy, produced by Pratt & Whitney Aircraft, Goverment Products Div. was examined in a JE0L 2000FX AEM. Both electropolished thin sections, and extraction replicas were examined to characterize this material. The consolidation procedure for producing this material included a 9:1 extrusion at 340°C followed by a 16:1 extrusion at 400°C, utilizing RS powders which have also been characterized utilizing electron microscopy.


1918 ◽  
Vol 86 (2218supp) ◽  
pp. 11-11
Author(s):  
Frank McManamy
Keyword(s):  

1918 ◽  
Vol 86 (2225supp) ◽  
pp. 123-123
Keyword(s):  

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