Revistas
Artículos
Publicaciones
Documentos
REVISTA
Applied and Computational Mechanics
TODAS
Redirigiendo al acceso original de articulo en
24
segundos...
Inicio
/
Applied and Computational Mechanics
/
Vol: 4 Núm: 1 Par: 0 (2010)
/
Artículo
ARTÍCULO
TITULO
Shape optimization of supersonic ejector for supersonic wind tunnel
Václav Dvorák
Resumen
s-
Acceso
PÁGINAS
NÚMERO
Volumen: 4 Número: 1 Parte: 0 (2010)
MATERIAS
INGENIERÍA Y CONSTRUCCIÓN CIVIL
TECNOLOGÍA
REVISTAS SIMILARES
Aerospace
Artículos similares
Experimental Investigation of Flameholding in Scramjet Combustor by Pylon with Plasma Actuator Based on Q-DC Discharge
Acceso
Aleksandr A. Firsov
This paper presents the results of testing and optimization of a plasma-assisted combustion scheme based on a pylon for fuel injection equipped with a plasma actuator. Electrodes were installed behind the stern of the pylon for the creation of Q-DC disch...
ver más
Revista:
Aerospace
Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and Actuators
Acceso
Chang-Yull Lee and Ji-Hwan Kim
A smart-skin antenna structure is investigated for active flutter control with piezoelectric sensors and actuators. The skin antenna is designed as a multilayer sandwich structure with a dielectric polymer to perform the role of antenna or radar structur...
ver más
Revista:
Aerospace
Supersonic Compressor Cascade Shape Optimization under Multiple Inlet Mach Operating Conditions
Acceso
Marco Casoni, Andrea Magrini and Ernesto Benini
Transonic compressors are widely used today in propulsion and industrial applications thanks to their higher specific work compared to subsonic. In this work, the aerodynamic optimization of a two-dimensional Computational Fluid Dynamics (CFD) model of t...
ver más
Revista:
Aerospace
Influence of Nozzle Exit Conditions on the Near-Field Development of High Subsonic and Underexpanded Axisymmetric Jets
Acceso
Miles T. Trumper, Parviz Behrouzi and James J. McGuirk
Detailed knowledge of jet plume development in the near-field (the first 10?15 nozzle exit diameters for a round jet) is important in aero-engine propulsion system design, e.g., for jet noise and plume infrared (IR) signature assessment. Nozzle exit Mach...
ver más
Revista:
Aerospace
Revistas destacadas
Infrastructures
Informed Infraestructure
BiT
Revista de la Construcción
Ver todas las revistas