Research Paper > IIT Bombay - AEROSPACE AE 628Intakes Nozzles


Aerodynamics ofIntakes and Propelling NozzlesTheory and Design2Requirements made on the inlets and nozzles:Both1. Minimize installation drag on their own and adjacentaircraft surfaces over wide range of aircraft angle ofattack and engine throttle settings2. Maximize internal total pressure recovery (πd, πn ) ofIntake and nozzle individually under variousoperating conditions3. Provide controllabl ...[Show More]

Preview 1 out of 43 pages
Purchase this document to unlock the blurred part and the rest of the document

Unlock Now

Reviews( 0 )