Results 261 to 270 of about 10,509 (314)

Aerodynamic calculation of unmanned aircraft

Aircraft Engineering and Aerospace Technology, 2005
PurposeTo provide an effective numerical method for analysis and design of aerodynamic characteristics of unmanned aerial vehicles basing on commercial package VSAERO.Design/methodology/approachCalculation was made by VSAERO package, which is based on a classical panel method enhanced on boundary layer method.
Marcin Figat   +2 more
openaire   +1 more source

Method of calculation of aerodynamic and acoustic characteristics of aerodynamic profiles

2023
The paper considers the theory of explaining the physical mechanisms of the occurrence of the trailing edge aerodynamic tonal noise of the airfoils. An analysis of the possibilities of using the ANSYS FLUENT software package for direct calculation of the aerodynamic and acoustic characteristics of airfoils in the near field is carried out using the ...
Mamuzić, Ilija   +3 more
openaire   +2 more sources

Parametric Calculations of the Aerodynamics of a Descent Vehicle

Herald of the Bauman Moscow State Technical University. Series Natural Sciences, 2021
We present the methodology and results of parametric aerodynamic studies of vehicles descending into the planet’s atmosphere. The proposed computational approach might serve as the basis for solving a number of problems such as predicting and optimizing the descent trajectory of the vehicle, the search for a rational aerodynamic layout of the vehicle ...
V.N. Dubovik   +5 more
openaire   +1 more source

Instruction Manual for the Aerodynamic Lens Calculator

Aerosol Science and Technology, 2006
This is an instruction manual for the aerodynamic lens design tool: the “Aerodynamic Lens Calculator”. We explain how to install and use this software. Examples are provided to use this tool to design or test a lens system. The structures of the source code programming are also provided in this manual.
Xiaoliang Wang, Peter H. McMurry
openaire   +1 more source

Application of Emergent Aerodynamic Calculation Tools

SAE Technical Paper Series, 2008
<div class="htmlview paragraph">The cost of fuel and the desire for fuel efficiency continue to drive automobile manufacturers to invest in and to prioritize vehicle designs and performance. There has long been a fundamental understanding that aerodynamic efficiency (drag) has an effect on this phenomenon.
Kurt A. Zielinski, Jonathan Eccles
openaire   +1 more source

Numerical Calculation of a Missile's Aerodynamic Characteristic

Advanced Materials Research, 2011
In virtue of Fluent of CFD software, numerical computations of aerodynamics of an air-to-air missile in different mach numbers and different attack angles were carried though. The movement trends of lift coefficient, drag coefficient and pitching moment coefficient with variety of mach numbers and attack angles were gained, meanwhile, distributing ...
Chun Guo Yue   +3 more
openaire   +1 more source

Methodology for calculating aerodynamic sensitivity derivatives

AIAA Journal, 1992
Summary: A general procedure is developed for calculating aerodynamic sensitivity coefficients using the full equations of inviscid fluid flow, where the focus of the work is the treatment of geometric shape design variables. Using an upwind cell-centered finite volume approximation to represent the Euler equations, sensitivity derivatives are ...
Taylor, Arthur C. III.   +2 more
openaire   +2 more sources

Calculation Methods for Aerodynamic Flows—a Review

1986
The present volume has been arranged so as to emphasize present abilities to calculate flows involving three independent variables and, at the same time to provide a background of the two-dimensional approaches upon which they are based. In the earlier review by Cebeci, Stewartson, and Whitelaw [1], two-dimensional flows were considered in some detail,
Tuncer Cebeci, J. H. Whitelaw
openaire   +1 more source

Progress in high-lift aerodynamic calculations

31st Aerospace Sciences Meeting, 1993
The current work presents progress in the effort to numerically simulate the flow over high-lift aerodynamic components, namely, multi-element airfoils and wings in either a take-off or a landing configuration. The computational approach utilizes an incompressible flow solver and an overlaid chimera grid approach.
openaire   +1 more source

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