Beschreibung
The book deals with determining the performance of the wing having a morphed trailing edge over the wing having slotted trailing edge. Since the phenomenon of morphing provides advantages such as changing the shape, improving the aerodynamic stability, aerodynamic coefficients and performance of the aircraft depending on the requirement at any time, its usage appears to be beneficial to be used in Aircraft.
Autorenporträt
Mr. Amit Kumar R., and Mrs.Kanu Priya Jhanji currently working as Assistant Professor in School of Aeronautical Sciences, Hindustan Institute of Technology and Science. Both the authors have obtained their Master's degree in Aeronautical Engineering and has authored technical papers in Aerodynamics and Composite materials.
Herstellerkennzeichnung:
OmniScriptum SRL
Str. Armeneasca 28/1, office 1
2012 Chisinau
MD
E-Mail: info@omniscriptum.com
