A computational study of multiple jet and wall interaction [PDF]
In the fuel preburner of the Space Shuttle Main Engine, face plate, injector, and baffle erosion have been observed. The observed patterns of erosion suggest that flame attachment to the walls is a contributing factor.
Campbell, W.
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A new aircraft architecture based on the ACHEON Coanda effect nozzle: flight model and energy evaluation [PDF]
, 2016 Michele Trancossi +13 more
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The further development of circulation control airfoils [PDF]
The performance trends of circulation control airfoils are reviewed and observations are made as to where improvements in performance and expansion of the flight envelope may be feasible. A new analytically defined family of airfoils is suggested, all of
Wood, N. J.
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Fluidics Thrust Vectoring Using Co-Flow Method
مجلة النهرين للعلوم الهندسية, 2017 Computational and experimental investigations of thrust vectoring using co flow method had been carried in the present work. The experimental investigation included design and construction of rig with rectangular duct with aspect ratio (4.4) in order to ...
Ali Abdul Almuhsen Al-Asady +1 more
doaj
Airstream Deflection Across a Cylindrical Surface
International Scholastic Journal of Science, 2016 A cylindrical airstream was blown across a cylindrical surface. The deflection angle, peak speed, and asymmetry of the airstream were measured while changing the location of the cylinder relative to the center of the wind column, and while changing the ...
Aydin Yolar
doaj
Exploratory studies of the cruise performance of upper surface blown configurations. Experimental program: Test facilities, model design instrumentation, and lowspeed, high-lift tests [PDF]
The model hardware, test facilities and instrumentation utilized in an experimental study of upper surface blown configurations at cruise is described.
Braden, J. A. +3 more
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Aerodynamic characteristics of circulation control airfoils with Magnus rotating cylinder
Engineering Applications of Computational Fluid MechanicsIn the aerodynamic performance optimization for aircraft, although both the Magnus effect and the Coanda effect have demonstrated significant potential increasing lift, reducing drag, and enabling flow control, the complex flow mechanisms arising from ...
Yunlong Zhao +5 more
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Kestrel Results at Liftoff Conditions for a Space Launch System Configuration in Proximity to the Launch Tower [PDF]
Aerodynamic data books for Space Launch System vehicles require databases for the integrated forces and moments and section loads during liftoff and transition to the ascent phase of flight.
Ghaffari, Farhad +3 more
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Theoretical predictions of jet interaction effects for USB and OWB configurations [PDF]
A wing jet interaction theory is presented for predicting the aerodynamic characteristics of upper surface blowing and over wing blowing configurations. For the latter configurations, a new jet entrainment theory is developed.
Campbell, J. F., Lan, C. E.
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