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This Book is based on conceptual Design of A 150 seater jet airplane cruising at M = 0.8, at 11 km altitude and having a gross still air range(GSAR) of 4000 km is considered$. The presentation is divided into eight sections - Data collection - Preliminary weight estimation - Optimization of wing loading and thrust loading - Wing design - Fuselage design, preliminary design of tail surface and preliminary layout - c.g. calculations - Revised estimates of areas of horizontal and vertical tails - Features of designed airplane - Details of performance estimation

Produktbeschreibung
This Book is based on conceptual Design of A 150 seater jet airplane cruising at M = 0.8, at 11 km altitude and having a gross still air range(GSAR) of 4000 km is considered$. The presentation is divided into eight sections - Data collection - Preliminary weight estimation - Optimization of wing loading and thrust loading - Wing design - Fuselage design, preliminary design of tail surface and preliminary layout - c.g. calculations - Revised estimates of areas of horizontal and vertical tails - Features of designed airplane - Details of performance estimation
Autorenporträt
Mr. Navdeep Banga is junior Research scholar from India. He specializes in Aircraft Design and experiments in flight. Author completed his Bachelor in technology in Aerospace engineering. He has four research publication in prestigious international journals. he also having experience in aircraft maintenance and airworthiness requirements.