Results 121 to 130 of about 4,183,596 (242)

Mean flow characteristics for the oblique impingement of an axisymmetric jet [PDF]

open access: yes
The oblique impingement of an axisymmetric jet has been investigated. A summary of the data and the analytical interpretations of the dominant mechanisms which influence the flow are reported.
Foss, J. F., Kleis, S. J.
core   +1 more source

Experimental Investigation of Ionization Sensors Under Shock Tube Stagnation Conditions

open access: yesJournal of Aerospace Technology and Management, 2017
Recently, there has been a growing interest in studies concerning ionization sensors for aerospace applications, power generation, and fundamental research. In aerospace research, they have been used for studies of shock and detonation waves.
Rafael Augusto Cintra   +2 more
doaj  

High Reynolds Number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel [PDF]

open access: yes
A wind-tunnel investigation of the NASA SC(2)-0012 airfoil has been conducted in the Langley 0.3-Meter Transonic Cryogenic Tunnel. This investigation supplements the two-dimensional airfoil studies of the Advanced Technology Airfoil Test Program.
Lawing, Pierce L., Mineck, Raymond E.
core   +1 more source

Straining Flow Effects on Sperm Flagellar Energetics in Microfluidic Cross-Slot Traps. [PDF]

open access: yesSmall
Javaherchian J   +4 more
europepmc   +1 more source

Uncertainty analysis of turbine nozzle guide vane cooling performance. [PDF]

open access: yesPLoS One
Lou D   +5 more
europepmc   +1 more source

Asymmetric hypersonic flow [PDF]

open access: yes
A general method for the analysis of the inviscid asymmetric hypersonic flow fields enveloping smooth bodies of general shape is given. The method is based on the assumption of a thin shock layer which yields an expression for pressure in generalized ...
Maslen, S. H.
core   +1 more source

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