I trying to understand a different methodologies of initial sizing methodologies for aircraft , and i have problem to understand to Raymer methodology ( especially i am stuck in constraint diagram) .
Dear Matúš Michalík I can understand your confusion. Initially, we must fix the weight constraint of the flying vehicle then we will be able to calculate it's performance. The procedure explained by Raymer is little complicated, I suggest you to refer other books of Anderson, John D. Jr., Perkins, C. and Hage, R like:
Aircraft Performance and Design
Introduction to Flight, McGraw-Hill
Airplane Performance, Stability and Control
Also you can see these research articles:
Thesis Detailed Design of 120 Seater Passenger Aircraft _Aircraft D...
Thesis Design of 120 Seater Passenger Aircraft _Aircraft Design Project-I
Thesis Aircraft Design Project (Detailed)_ Design of 100 Seater STO...