Unsteady aerodynamics
Resource Information
The concept Unsteady aerodynamics represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
The Resource
Unsteady aerodynamics
Resource Information
The concept Unsteady aerodynamics represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- Unsteady aerodynamics
- Source
- nasat
65 Items that share the Concept Unsteady aerodynamics
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- User's guide for MSAP2D : a program for unsteady aerodynamic and aeroelastic (flutter and forced response) analysis of multistage compressors and turbines : under grant NAG3-1137
- A historical overview of flight flutter testing
- ASTROP2 users manual : a program for aeroelastic stability analysis of propfans
- ASTROP2 users manual : a program for aeroelastic stability analysis of propfans
- Active control of flow separation over an airfoil
- Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
- Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
- Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data
- Airloads, wakes, and aeroelasticity
- An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation
- An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation
- An experimental and computational investigation of oscillating airfoil unsteady aerodynamics at large mean incidence
- Analysis of inlet-compressor acoustic interactions using coupled CFD codes
- Analysis of inlet-compressor acoustic interactions using coupled CFD codes
- Analysis of wind tunnel oscillatory data of the X-31A aircraft
- Application of approximate unsteady aerodynamics for flutter analysis
- Application of the ASP3D computer program to unsteady aerodynamic and aeroelastic analyses
- Assessment of JVX proprotor performance data in hover and airplane-mode flight conditions
- Basis function approximation of transonic aerodynamic influence coefficient matrix
- CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999
- Comparison of Theodorsen's unsteady aerodynamic forces with double lattice generalized aerodynamic forces
- Computational aeroservoelastic analysis with an Euler-based unsteady flow solver : NASA-Ames university consortium cooperative agreement no. NCC2-5105, final research summary for the period: 1 November 1994 - 31 January 1997
- Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
- Control of flow separation and mixing by aerodynamic excitation
- Development of a composite tailoring technique for airplane wing : progress report/renewal proposal, grant no. NAG2-908
- Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver
- Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver
- Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
- Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
- Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade
- Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade
- Experimental verification of buffet calculation procedure using unsteady PSP
- Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
- Fourier functional analysis for unsteady aerodynamic modeling
- Gust response analysis of a turbine cascade
- Gust response analysis of a turbine cascade
- Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
- Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
- Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines
- Initial assessment of the Ares I-X launch vehicle upper stage to vibroacoustic flight environments
- Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
- Linearized unsteady aerodynamic analysis of the acoustic response to wake/blade-row interaction
- Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade
- Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade
- Modeling of aircraft unsteady aerodynamic characteristics, Part 3, Parameters estimated from flight data
- Modeling of longitudinal unsteady aerodynamics of a wing-tail combination
- Modeling of unsteady three-dimensional flows in multistage machines
- Numerical simulation methods of incompressible flows and an application to the space shuttle main engine
- Numerical study of steady and unsteady canard-wing-body aerodynamics
- Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack
- Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
- Semi-annual status report on NASA grant NAG 1-1087 : "identification of aerodynamic models for maneuvering aircraft"
- Sensitivity analysis of flutter response of a wing incorporating finite-span corrections
- Structural Dynamics Division research and technology accomplishments for FY 1989 and plans for FY 1990
- System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality : a dissertation ...
- System identification and POD method applied to unsteady aerodynamics
- Technical evaluation report on unsteady aerodynamics--fundamentals and applications to aircraft dynamics
- The effect of wake passing on turbine blade film cooling
- The effect of wake passing on turbine blade film cooling
- Three-dimensional Euler time accurate simulations of fan rotor-stator interactions
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Unsteady aerodynamic model tuning for precise flutter prediction
- Unsteady aerodynamics : subsonic compressible inviscid case
- Unsteady cascade aerodynamic response using a multiphysics simulation code
- Unsteady cascade aerodynamic response using a multiphysics simulation code
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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.umsl.edu/resource/b6bhbFXFFNM/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/b6bhbFXFFNM/">Unsteady aerodynamics</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
