Characterization of Inhalation Exposure to Jet Fuel among U.S. Air Force Personnel

2012 ◽  
Keyword(s):  
Air Force ◽  
Inhalation Exposure ◽  
Jet Fuel

Characterization of Jet Fuel Inhalation Exposure and Urinary Metabolites in U.S. Air Force Personnel

Epidemiology ◽  
2009 ◽  
Vol 20 ◽  
pp. S60
Author(s):  
Ema Rodrigues ◽  
Kian Merchant-Borna ◽  
Kristen Smith ◽  
Susan Proctor ◽  
Michael McClean
Keyword(s):  
Air Force ◽  
Inhalation Exposure ◽  
Urinary Metabolites ◽  
Jet Fuel

Inhalation Exposure to Jet Fuel (JP8) Among U.S. Air Force Personnel

2010 ◽  
Vol 7 (10) ◽  
pp. 563-572 ◽  
Author(s):  
Kristen W. Smith ◽  
Susan P. Proctor ◽  
Al Ozonoff ◽  
Michael D. McClean
Keyword(s):  
Air Force ◽  
Inhalation Exposure ◽  
Jet Fuel

Characterization of High Altitude Turbulence for Air Force Platforms

2007 ◽  
Author(s):  
Frank H. Ruggiero ◽  
Joseph A. Werne ◽  
Alex Mahalov ◽  
Basil Nichols ◽  
Donald E. Wroblewski
Keyword(s):  
High Altitude ◽  
Air Force

Synthesis and characterization of esters from different alcohols using Macauba almond oil to substitute diesel oil and jet fuel

Fuel ◽  
2016 ◽  
Vol 166 ◽  
pp. 453-460 ◽  
Author(s):  
Larissa Noemi Silva ◽  
Claudia Cristina Cardoso ◽  
Vânya M.D. Pasa
Keyword(s):  
Diesel Oil ◽  
Jet Fuel ◽  
Synthesis And Characterization ◽  
Almond Oil

Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor

1988 ◽  
Vol 110 (3) ◽  
pp. 386-392 ◽  
Author(s):  
D. C. Rabe ◽  
A. J. Wennerstrom ◽  
W. F. O’Brien
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Air Force ◽  
Leading Edge ◽  
Transonic Compressor ◽  
Laser Measurements ◽  
Compressor Rotor ◽  
Boundary Layer Interaction ◽  
Air Force Base

The passage shock wave–endwall boundary layer interaction in a transonic compressor was investigated with a laser transit anemometer. The transonic compressor used in this investigation was developed by the General Electric Company under contract to the Air Force. The compressor testing was conducted in the Compressor Research Facility at Wright-Patterson Air Force Base, OH. Laser measurements were made in two blade passages at seven axial locations from 10 percent of the axial blade chord in front of the leading edge to 30 percent of the axial blade chord into the blade passage. At three of these axial locations, laser traverses were taken at different radial immersions. A total of 27 different locations were traversed circumferentially. The measurements reveal that the endwall boundary layer in this region is separated from the core flow by what appears to be a shear layer where the passage shock wave and all ordered flow seem to end abruptly.

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