Концептуальное проектирование самолетов. — Samara: Samara State Aerospace University; 2011. — 37 р.Guide is an example of a term project on discipline Conceptual aircraft design for the specialties 160201 Airplane and Helicopter Construction, 160901 Technical Maintenance of Aircrafts and Engines and for the Masters programme «Designing, construction and CALS-technologies in Aeronautical Engineering» for education direction 160100.68 «Aeronautical Engineering».
Prepared by the Department of Aeronautical Engineering SSAU.Contents
Statistics analysis
Scientific and technological forecasting
Analysis of the project situation
Development of initial specification
General technical requirements
Aircraft performance requirements
Production and technological requirements
Performance Requirements
The technical and economic requirements
Baseline configuration development
Selection of the wing parameters
Selection of the fuselage parameters
The choice of the tail parameters
Selection of the control surfaces parameters
Selection of the undercarriage parameters
The relative position of the aircraft units
Selection of the propulsion system
Selecting the number of engines and their placement on the aircraft
Determination of initial aircraft parameters
Determination of the specific load on the wing
Aerodynamic parameters
Identification of aircraft thrust needs
Determination of aircraft takeoff weight
Definition of the initial take-off weight
Definition of the payload mass
Definition of the equipment mass and service load
Determination of the relative weight of construction
Determination of relative weight of the fuel system
Determination of the relative masses of powerplant
Determination of relative weight of the equipment and controls
Definition of take-off weight of the first approximation
Determination of the absolute dimensions of the aircraft
Selection of engines
Determination of the fuel mass and volume
Specifying the wing parameters
Definition of the plumage parameters
Determination of the fuselage dimensions
Determination of the undercarriage parameters
Aircraft weight estimation
Wight summary
Aicraft layout
Aircraft volume-weight assembly
The structural layout of the aircraft
Aircraft balance
Choice of balance range
Specified loading conditions
Development of a general drawing view and aircraft technical description
Conclusion
Bibliography
