Author: J. R. Frahm
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
An Approach to Environmental Control System Weight Estimation in Advanced Design
Author: J. R. Frahm
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
Airplane Design
Author: Jan Roskam
Publisher: DARcorporation
ISBN: 9781884885525
Category : Technology & Engineering
Languages : en
Pages : 598
Book Description
Publisher: DARcorporation
ISBN: 9781884885525
Category : Technology & Engineering
Languages : en
Pages : 598
Book Description
Lawyers Desk Reference
Author:
Publisher:
ISBN:
Category : Accident law
Languages : en
Pages : 552
Book Description
Publisher:
ISBN:
Category : Accident law
Languages : en
Pages : 552
Book Description
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 314
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 314
Book Description
Space Station Systems
Author:
Publisher:
ISBN:
Category : Space stations
Languages : en
Pages : 652
Book Description
Publisher:
ISBN:
Category : Space stations
Languages : en
Pages : 652
Book Description
Weights of Environmental-control Systems
Author: Stephen H. Dole
Publisher:
ISBN:
Category : Life support systems (Space environment)
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category : Life support systems (Space environment)
Languages : en
Pages : 0
Book Description
Large Space Structures & Systems in the Space Station Era
Author:
Publisher:
ISBN:
Category : Large space structures (Astronautics)
Languages : en
Pages : 368
Book Description
Publisher:
ISBN:
Category : Large space structures (Astronautics)
Languages : en
Pages : 368
Book Description
Influence of flight control laws on structural sizing of commercial aircraft
Author: Rahmetalla Nazzeri
Publisher: Cuvillier Verlag
ISBN: 3736965168
Category : Technology & Engineering
Languages : en
Pages : 180
Book Description
The increasing demand for new civil aircraft pushes aircraft manufacturers to develop innovative solutions that lead in particular to mass reductions. One way to achieve these kinds of improvements is the use of multidisciplinary analysis and optimization. In this sense the intention of this PhD thesis is to develop a multidisciplinary framework in order to quantify the impact of load alleviation function parameter changes on structural components like the wing and fuselage in terms of resulting mass changes. The developed iterative process chain covers the loads calculation including an active load alleviation system, a structural assessment of the wing and fuselage components and a dedicated feedback loop in order to update mass and stiffness properties of the loads calculation model. The study shows that significant mass reductions are achievable while on the other hand estimated mass penalties are irrelevant.
Publisher: Cuvillier Verlag
ISBN: 3736965168
Category : Technology & Engineering
Languages : en
Pages : 180
Book Description
The increasing demand for new civil aircraft pushes aircraft manufacturers to develop innovative solutions that lead in particular to mass reductions. One way to achieve these kinds of improvements is the use of multidisciplinary analysis and optimization. In this sense the intention of this PhD thesis is to develop a multidisciplinary framework in order to quantify the impact of load alleviation function parameter changes on structural components like the wing and fuselage in terms of resulting mass changes. The developed iterative process chain covers the loads calculation including an active load alleviation system, a structural assessment of the wing and fuselage components and a dedicated feedback loop in order to update mass and stiffness properties of the loads calculation model. The study shows that significant mass reductions are achievable while on the other hand estimated mass penalties are irrelevant.
Airplane Design: Preliminary configuration design and integration of the propulsion system
Author: Jan Roskam
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 344
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 344
Book Description