Fluid flow studies of the F-5E and F-16 inlet ducts

• المؤلف الرئيسي: Imran Halimi Ibrahim
• مؤلفون آخرون: Ng Yin Kwee
• التنسيق: Theses and Dissertations
• اللغة: English
• منشور في: 2009
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Jet propulsion
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/14581

The intake represents the front of a complex aerodynamic system. The shape of the intake diffuser follows the contours of the aircraft for external aerodynamic reasons. However the meandering shape can result in unwanted secondary flow or swirl build up at the Aerodynamic Interface Plane (AIP), resu...