Abstract: The synthetic fuel industry is poised to experience largescale growth and profoundly affect current aviation fuel infrastructure. New candidate technologies, such as Camelina oilderived synthetic fuel have been demonstrated ...

Abstract: This work details an experimental investigation on the effects of the variation of flap gap and overlap sizes on the flow field in the wake of a wing-section equipped with a trailing edge Fowler flap. The airfoil was based ...

Abstract: A durability test rig for erosionresistant gas turbine engine compressor blade coatings was designed and commissioned. Bare and coated 174PH steel modified NACA 6505profile blades were spun at an average speed of 10,860 rpm ...

Abstract: Performance differences between bare 174PH steel V103 profile (NACA 6505 with rounded leading edge (LE) and trailing edge (TE)) gas turbine engine axial compressor blades, and those coated with either a chromiumaluminumtitanium ...

Abstract: This paper reports the internal performance evaluation of S-duct diffusers with different entrance aspect ratios as part of a parametric investigation of a generic S-duct inlet. The generic S-duct diffusers studied had a ...