Analysis of nozzle for the external casing perforation tool and experimental study on AWJ. [PDF]
Ren X, Zhu W, Che Y, Yao J.
europepmc +1 more source
Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser [PDF]
An investigation has been conducted in the static-test facility of the Langley 16-Foot Transonic Tunnel to determine the effects of reverser port geometry on the internal performance of a nonaxisymmetric rotating-vane-type thrust reverser.
Berrier, B. L., Capone, F. J.
core +1 more source
A novel approach to develop the turning tool for cryogenic internal cooling. [PDF]
Gan Y +5 more
europepmc +1 more source
Integrated transient thermal-structural finite element analysis [PDF]
An integrated thermal structural finite element approach for efficient coupling of transient thermal and structural analysis is presented. Integrated thermal structural rod and one dimensional axisymmetric elements considering conduction and convection ...
Dechaumphai, P. +3 more
core +1 more source
Thrust Vector Control of Non-axisymmetric Nozzles
Article
openaire
Passive control of suddenly expanded flow and temperature distribution along the duct at critical Mach number. [PDF]
Tamboli S +8 more
europepmc +1 more source
Performance of twin two-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20 [PDF]
Transonic tunnel and supersonic pressure tunnel tests were reformed to determine the performance characteristics of twin nonaxisymmetric or two-dimensional nozzles with fixed shrouds and variable-geometry wedges.
Capone, F. J., Maiden, D. L.
core +1 more source
Fabricating High Aspect Ratio Amorphous Alloys Microgrooves by Using Periodically Thinning Jet Electrochemical Milling Method. [PDF]
Li Y, Ming P, Li D, Zhao R, Niu S.
europepmc +1 more source
OH* 3D Concentration Measurement of Non-Axisymmetric Flame via Near-Ultraviolet Volumetric Emission Tomography. [PDF]
Ma J +5 more
europepmc +1 more source
Characteristic variation of Mach number in subsonic co-flowing jets by varying lip thickness. [PDF]
Kumar KS +5 more
europepmc +1 more source

