Results 31 to 40 of about 251 (111)
This paper presents an integrated simulation framework for assessing air‐to‐air engagement effectiveness, accounting for missile guidance dynamics, target motion, radar signal processing, and target vulnerability to warhead effects. The proposed approach combines models of missile‐target interaction, radar cross‐section (RCS)‐based signal processing ...
Witold Bużantowicz, Kamil Klicki
wiley +1 more source
A mathematical model and software for online modeling of the parameters and characteristics of a cruise missile with a pulsejet engine to evaluate the potential use of this type of engine in high‐speed unmanned aerial vehicles (UAVs) were developed. The model describes the acceleration after launch and the steady horizontal flight of a cruise missile ...
Alexander Khrulev +2 more
wiley +1 more source
Dimensionless Groups by Entropic Similarity: II-Wave Phenomena and Information-Theoretic Flow Regimes. [PDF]
Niven RK.
europepmc +1 more source
Application of panel methods for subsonic aerodynamics
Several panel methods are developed to model subsonic aerodynamics. The vorticity panel method for two-dimensional problems is capable of handling general unsteady, potential, lifting flows.
Kim, Meung Jung
core
INDUSTRIAL CFD SIMULATION OF AERODYNAMIC NOISE [PDF]
Real challenges to suppress undesirable fluid-excited acoustics are posed by a wide variety of engineering disciplines. Noise regulations, passenger comfort and component stability are motivators which are continuing to stimulate substantial efforts ...
Caridi, Domenico
core +1 more source
Assessing the impact of aerodynamic modelling on manoeuvring aircraft
This paper investigates the impact of aerodynamic models on the dynamic response of a free-flying aircraft wing. Several options for the aerodynamics are evaluated, from two-dimensional thin aerofoil aerodynamics and unsteady vortex-lattice method up to ...
Hesse, H. +16 more
core +1 more source
Topics in Numerical Computation of Compressible Flow [PDF]
This thesis aims to assist the development of a multiblock implicit Navier-Stokes code for hypersonic flow applications. There are mainly three topics, which concern the understanding of basic Riemann solvers, the implementing of implicit zonal ...
Lin, Hong-Chia
core +2 more sources
The finite element method in low speed aerodynamics [PDF]
The finite element procedure is shown to be of significant impact in design of the 'computational wind tunnel' for low speed aerodynamics. The uniformity of the mathematical differential equation description, for viscous and/or inviscid, multi ...
Manhardt, P. D., Baker, A. J.
core
Dataset of numerical simulations for aeroelastic control of an aero engine compressor cascade using plasma actuators. [PDF]
De Giorgi MG +3 more
europepmc +1 more source
Numerical study on the influence of wall temperature gradient on aerodynamic characteristics of low aspect ratio flying wing configuration. [PDF]
Lin P +6 more
europepmc +1 more source

