Rotorcraft fuselage mass assessment in early design stages
نویسندگان
چکیده
منابع مشابه
Parametric Fuselage Geometry Generation and Aerodynamic Performance Prediction in Preliminary Rotorcraft Design
The creation of an integrated rotorcraft conceptual and preliminary design framework at DLR involved the development of geometry and fuselage aerodynamics modules at the Institute of Aerodynamics and Flow Technology. After a short revision of the RIDE rotorcraft design environment architecture this paper focuses on the implementation of these disciplinary modules. The aim of the geometry module...
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ژورنال
عنوان ژورنال: CEAS Aeronautical Journal
سال: 2021
ISSN: 1869-5582,1869-5590
DOI: 10.1007/s13272-021-00492-z