Pasquale Sforza, Theory of Aerospace Propulsion, Butterworth-Heinemann (2011)Pasquale M. Sforza. Theory of Aerospace Propulsion. Elsevier Scientific Pub. Co., 2011.Sforza, P.M.: Theory of Aerospace Propulsion. Academic Press, Waltham (2012)
推荐 内容简介· ··· Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies...
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Theory of Aerospace Propulsionprovides excellent coverage of aerospace propulsion systems, including propellers, nuclear rockets, and space propulsion. The book’s in-depth, quantitative treatment of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal...
5 theory of aerospace propulsion provides excellent coverage of aerospace propulsion systems, including propellers, nuclear rockets, and space propulsion. the book's in-depth, quantitative treatment of the components of jet propulsion engines provides the tools for evaluation and component matching for ...
1 航空宇航推进理论与工程(AerospacePropulsionTheoryandEngineering)(硕士点) 浙江大学“航空宇航推进理论与工程”作为我校航空宇航科学与技术领域下属的二级学科 之一,依托航空航天学院航空航天系和工程力学系的师资力量和科研教学环境,聚集了一支由长 江特聘教授和求是特聘教授领导的不断壮大的科研教学队伍。
, (1954) "The Elementary Theory of Aero‐Elasticity: A Series of Articles Written from the Standpoint of a Structural Engineer for Students and Junior Members of Aircraft Design Teams", Aircraft Engineering and Aerospace Technology, Vol. 26 Iss: 4, pp.113 - 121 DOI http://dx.doi.org/...
Users only need to click on these icons or hyperlinks to view detailed explanations of corresponding entries in the "Large Device Library". Do not remind me again Cancel Confirm Abstract We report for the first time that in heterotic string compactified on 4-torus or equivalently IIA string ...
A discussion of limitations and future directions of the methodology is included. The methodology, in a more complicated form, is used primarily for hypersonic sonic boom prediction. Paper Link [PDF] Posted bysaemillerJanuary 9, 2025Posted inAeronautics, Aerospace, Computing, Fluid Dynamics, ...
Based on the assumption of multiple time scale separation, a zeroth-order closed-form solution is obtained, enabling one to use realistic aerodynamic and propulsion data. Control strategies are approximated by explicit feedback expressions of the state variables and the aircraft performance parameters. ...