Aerodynamics -- Mathematical models
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The concept Aerodynamics -- Mathematical models represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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Aerodynamics -- Mathematical models
Resource Information
The concept Aerodynamics -- Mathematical models represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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- Aerodynamics -- Mathematical models
- Authority link
- (EG-IN)1087935
31 Items that share the Concept Aerodynamics -- Mathematical models
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- User's manual for an aerodynamic optimization scheme that updates flow variables and design parameters simultaneously
- A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects
- A generalized orthogonal coordinate system for describing families of axisymmetric and two-dimensional bodies
- A methodology for airplane parameter estimation and confidence interval determination in nonlinear estimation problems
- A review of the analytical simulation of aircraft crash dynamics
- Aerodynamic preliminary analysis system II
- An analysis of prop-fan/airframe aerodynamic integration
- An efficient method for solving the steady Euler equations
- Analysis of pressure distortion testing
- Application of a new K-[tau] model to near wall turbulent flows
- Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies
- Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86
- Choice of implicit and explicit operators for the upwind differencing method
- Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies
- Computational methods for vortex dominated compressible flows : final report
- Derivation and definition of a linear aircraft model
- Development and validation of a combined rotor-fuselage induced flow-field computational method
- Development of MCAERO wing design panel method with interactive graphics module
- Identification of aerodynamic models for maneuvering aircraft : final report on NASA grant NAG 1-1087
- Identification of aerodynamic models for maneuvering aircraft : semi-annual status report on NASA grant NAG 1-1087
- Mathematical modeling of the aerodynamic characteristics in flight dynamics
- Modeling aerodynamic discontinuities and the onset of chaos in flight dynamical systems
- Nonlinear potential analysis techniques for supersonic/hypersonic configuration design
- Panel methods : an introduction
- Software reliability : additional investigations into modeling with replicated experiments
- Some aspects of essentially nonoscillatory (ENO) formulations for the Euler equations
- Sonic-boom wave-front shapes and curvatures associated with maneuvering flight
- Study of the integration of wind tunnel and computational methods for aerodynamic configurations
- Surrogate-equation technique for simulation of steady inviscid flow
- User's guide to PMESH : a grid-generation program for single-rotation and counterrotation advanced turboprops
- User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/kuMceT8geSI/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/kuMceT8geSI/">Aerodynamics -- Mathematical models</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
