Results 101 to 110 of about 17,927 (212)

Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser [PDF]

open access: yes
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

Integrated transient thermal-structural finite element analysis [PDF]

open access: yes
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

open access: yesThrust 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]

open access: yesSci Rep
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]

open access: yes
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

Characteristic variation of Mach number in subsonic co-flowing jets by varying lip thickness. [PDF]

open access: yesSci Rep
Kumar KS   +5 more
europepmc   +1 more source

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