Shape memory alloy based morphing aerostructures
FT Calkins, JH Mabe - 2010 - asmedigitalcollection.asme.org
In order to continue the current rate of improvements in aircraft performance, aircraft and
components which are continuously optimized for all flight conditions, will be needed …
components which are continuously optimized for all flight conditions, will be needed …
Evolution from 'tabs' to 'chevron technology'-a review
K Zaman, JE Bridges, DL Huff - International Journal of …, 2011 - journals.sagepub.com
'Chevrons', a sawtooth pattern on the trailing edge of exhaust nozzles, are being
implemented on modern jet engines. The technology reduces jet noise for 'separate …
implemented on modern jet engines. The technology reduces jet noise for 'separate …
Lift-up, Kelvin–Helmholtz and Orr mechanisms in turbulent jets
Three amplification mechanisms present in turbulent jets, namely lift-up, Kelvin–Helmholtz
and Orr, are characterized via global resolvent analysis and spectral proper orthogonal …
and Orr, are characterized via global resolvent analysis and spectral proper orthogonal …
Boeing's variable geometry chevron, morphing aerostructure for jet noise reduction
J Mabe, F Calkins, G Butler - 47th AIAA/ASME/ASCE/AHS/ASC …, 2006 - arc.aiaa.org
Variable Geometry Chevrons were successfully flight tested on a Boeing 777-300ER with
GE-115B engines, demonstrating full-scale aerostructure morphing using shape memory …
GE-115B engines, demonstrating full-scale aerostructure morphing using shape memory …
Transforming the shock pattern of supersonic jets using fluidic injection
Double shock diamonds establish in the exhaust of modular convergent–divergent nozzles.
These consist of two shock structures: one originating from the nozzle throat, and another …
These consist of two shock structures: one originating from the nozzle throat, and another …
Flow control by dielectric barrier discharge actuators: jet mixing enhancement
THE control of the wake of axisymmetric jet flow has strong implications for a wide variety of
practical flows. The control of such flow primarily concerns military applications but also has …
practical flows. The control of such flow primarily concerns military applications but also has …
Variable geometry chevrons for jet noise reduction
F Calkins, G Butler, J Mabe - 12th AIAA/CEAS Aeroacoustics …, 2006 - arc.aiaa.org
Boeing is applying cutting edge smart material actuators to the next generation morphing
technologies for aircraft. This effort has led to the Variable Geometry Chevrons (VGC), which …
technologies for aircraft. This effort has led to the Variable Geometry Chevrons (VGC), which …
Boeing's variable geometry chevron: morphing aerospace structures for jet noise reduction
FT Calkins, JH Mabe, GW Butler - Smart Structures and …, 2006 - spiedigitallibrary.org
Boeing is applying cutting edge smart material actuators to the next generation morphing
technologies for aircraft. This effort has led to the Variable Geometry Chevrons (VGC), which …
technologies for aircraft. This effort has led to the Variable Geometry Chevrons (VGC), which …
Time-average measurement of velocity, density, temperature, and turbulence velocity fluctuations using Rayleigh and Mie scattering
AF Mielke, RG Seasholtz, KA Elam, J Panda - Experiments in fluids, 2005 - Springer
Measurement of time-averaged velocity, density, temperature, and turbulence velocity
fluctuations in sparsely seeded gas flows using a non-intrusive, point-wise technique based …
fluctuations in sparsely seeded gas flows using a non-intrusive, point-wise technique based …
Effect of chevron nozzle penetration on aero-acoustic characteristics of jet at M= 0.8
SR Nikam, SD Sharma - Fluid Dynamics Research, 2017 - iopscience.iop.org
Aero-acoustic characteristics of a high-speed jet with chevron nozzles are experimentally
investigated at a Mach number of 0.8. The main focus is to examine the effects of the extent …
investigated at a Mach number of 0.8. The main focus is to examine the effects of the extent …