The Effect of Wind Velocity on the Suppression of Composite Wing Airfoil NACA 0012
The first studies on shocks and vibrations were carried out at the beginning of the 1930s to improve the behavior of buildings during earthquakes. Vibration tests on aircraft were developed from 1940 to verify the resistance of parts and equipments prior to their first use. Flutter is a well-known...
Guardado en:
Autores principales: | Hassan Ali Kadhem, Ahmed Abdul Hussein |
---|---|
Formato: | article |
Lenguaje: | EN |
Publicado: |
Al-Khwarizmi College of Engineering – University of Baghdad
2019
|
Materias: | |
Acceso en línea: | https://doaj.org/article/c33c0fcd1a224689abc2163739ef50f7 |
Etiquetas: |
Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
Ejemplares similares
-
Assessment of several modeling strategies on the prediction of lift-drag coefficients of a NACA0012 airfoil at a moderate Reynold number
por: K.M. Almohammadi
Publicado: (2022) -
Effects of internal Acoustic Excitation on the Improvement of Airfoil Performance
por: Ikhlase M. Fayed
Publicado: (2007) -
Effects of internal Acoustic Excitation on the Improvementof Airfoil Performance
por: Ikhlase M.Fayed
Publicado: (2007) -
Effect of Adding Alcohols and Gas Velocity on Gas Hold up and Mass Transfer Coefficient in Bubble Columns with Draught Tube
por: Ali Abdul-Rahman N. Jasim
Publicado: (2009) -
Investigation of Load and Pressure Distribution on Wing with Wake Rollup for Low Speed Aircraft
por: Laith W. Ismail
Publicado: (2018)