Sectional Parametric Design and Aerodynamic Performance Estimation In Small Aircraft
نویسندگان
چکیده
منابع مشابه
Integrated Parametric Aircraft Design
Driven by the inspiration to develop a new aircraft that incorporates all fields of aeronautical engineering, the focal point of this designapproach is the geometric modelling. Since innovative technologies need to be included in novel configurations, every new idea has to be modelled in a comprehensible manner. Feedbacks coming from the analysed models are easily integrated in the next iterati...
متن کاملAerodynamic Analysis and Design of a Twin Engine Commuter Aircraft
The present paper deals with the preliminary design of a general aviation Commuter 11 seat aircraft. The Commuter aircraft market is today characterized by very few new models and the majority of aircraft in operation belonging to this category are older than 35 years. Tecnam Aircraft Industries and the Department of Aerospace Engineering (DIAS) of the University of Naples "Federico II" are dee...
متن کاملParametric 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...
متن کاملAn Aerodynamic Design Method for Supersonic Natural Laminar Flow Aircraft
The computation of boundary-layer properties and laminar-to-turbulent transition location is a complex problem generally not undertaken in the context of aircraft design. Yet this is just what must be done if an aircraft designer is to exploit the advantages of laminar flow while making the proper trade-offs between inviscid drag, structural weight and skin friction. To facilitate this process,...
متن کاملAerodynamic Design Optimization Studies of a Blended-Wing-Body Aircraft
Abstract The blended-wing body is an aircraft configuration that has the potential to be more efficient than conventional large transport aircraft configurations with the same capability. However, the design of the blended-wing is challenging due to the tight coupling between aerodynamic performance, trim, and stability. Other design challenges include the nature and number of the design variab...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: IOSR Journal of Engineering
سال: 2013
ISSN: 2278-8719,2250-3021
DOI: 10.9790/3021-03921724