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CZECH TECHNICAL UNIVERSITY IN PRAGUE
STUDY PLANS
2019/2020

Aerodynamic design of airplanes

The course is not on the list Without time-table
Code Completion Credits Range Language
2225021 KZ 3 2P+1C Czech
Lecturer:
Tutor:
Supervisor:
Department of Aerospace Engineering
Synopsis:

Lift characteristics of aircraft. Contribution of wing, body, horizontal tail areas and lift mechanics in the overall lift. The influence of Earth proximity on lift. Lift calculations within the bearing surface theory. Resistance characteristics of an aircraft, different components of resistance, contribution of different parts of the aircraft. Aircraft polar and its alternative forms. Moment characteristics of an aircraft (static stability), neutral point positioning. Influence of compressibility on lift, resistentce and moment characteristics. Characteristics of dynamic stability in longitudinal and side movements, aerodynamic derivation. Aircraft controlability, forces in control considering manageability and dexterity. Design of tail areas.

Requirements:

Fundamentals of Aerodynamics.

Syllabus of lectures:
Syllabus of tutorials:
Study Objective:

Know the basics of aerodynamic procedures when designing an aircraft.

Study materials:

E. Torenbeek: Synthesis of subsonic airplane design, Delft University, 1990

D. Küchemann: The aerodynamic design of aircraft, Pergamon Press, 1978

Note:
Further information:
No time-table has been prepared for this course
The course is a part of the following study plans:
Data valid to 2020-01-23
For updated information see http://bilakniha.cvut.cz/en/predmet1110006.html