#
Aerofoils
Resource Information
The concept ** Aerofoils** represents the subject, aboutness, idea or notion of resources found in **University of Missouri-St. Louis Libraries**.

The Resource
Aerofoils
Resource Information

The concept

**Aerofoils**represents the subject, aboutness, idea or notion of resources found in**University of Missouri-St. Louis Libraries**.- Label
- Aerofoils

## Context

Context of Aerofoils#### Subject of

No resources found

No enriched resources found

- A comparison of two central difference schemes for solving the Navier-Stokes equations
- A computer program for estimating the areodynamic characteristics of NACA 16-series airfoils
- A flow visualization study of the leading edge separation bubble on a NACA 0012 airfoil with simulated glaze ice
- A numerical study of the effects of wind tunnel wall proximity on an airfoil model
- A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations
- A turbulence model for iced airfoils and its validation
- Acoustic radiation from lifting airfoils in compressible subsonic flow
- Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section
- Aerodynamic characteristics of a rotorcraft airfoil designed for the tip region of a main rotor blade
- Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditions
- An Experimental investigation of a supercritical airfoil at transonic speeds
- An experimental investigation of the confluent boundary layer on a high-lift system : final project report
- An experimental mapping of the flow field behind a glaze ice shape on a NACA 0012 airfoil
- Artificial boundary conditions for computation of oscillating external flows
- Closed-loop separation control using oscillatory flow excitation
- Computation of full-coverage film-cooled airfoil temperatures by two methods and comparison with high heat flux data
- Computations of two-dimensional airfoil-vortex interactions
- Computer program to obtain ordinates for NACA airfoils
- Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel
- DRA/NASA/ONERA collaboration on icing research, Part II, Prediction of airfoil ice accretion
- Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift
- Development of form-adaptive airfoil profiles for wind turbine application
- Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model
- Effect of an extendable slat on the stall behavior of a VR-12 airfoil
- Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
- Estimation of unsteady lift on a pitching airfoil from wake velocity surveys
- Experimental ice shape and performance characteristics for a multi-element airfoil in the NASA Lewis Icing Research Tunnel
- Experimental investigation of the flowfield of an oscillating airfoil
- Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade
- Experimental investigations on airfoils with different geometries in the domain of high angles of attack - flow separation
- Experimental study of complex vortex interactions in the wake of high aspect ratio wings : final report on NASA grant NAG-1-1816
- Experimental verification of a new laminar airfoil : a project for the graduate program in aeronautics : final report
- Final report for modeling of heavy-gas effects on airfoil flows
- Flight Mechanics/Estimation Theory Symposium, 1989 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 23-24, 1989
- Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
- Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies
- Further wind tunnel investigation of the SM701 airfoil with aileron and turbulators
- Icing characteristics of a natural-laminar-flow, a medium-speed, and a swept,medium-speed airfoil
- Icing test results on an advanced two-dimensional high-lift multi-element airfoil
- Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
- Implementation of advanced two equation turbulence models in the USM3D unstructured flow solver
- Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction : final report
- Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction : semi-annual report for the period March 16, 1983 to September 14, 1983
- Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions
- Life prediction and constitutive models for engine hot section anisotropic materials program : annual status report
- Life prediction and constitutive models for engine hot section anisotropic materials program : final report
- Life prediction and constitutive models for engine hot section anisotropic materials program : second annual status report
- Materials for Advanced Turbine Engines (MATE) : project 4--erosion resistant compressor airfoil coating
- Modern airfoil ice accretions
- NASA supercritical airfoils : a matrix of family-related airfoils
- Navier-Stokes analysis of airfoils with leading edge ice accretions
- Numerical computation of viscous flow about unconventional airfoil shapes : final report
- Numerical modeling of anti-icing systems and comparison to test results on a NACA 0012 airfoil
- Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight
- Numerical solutions of the complete Navier-Stokes equations : progress report no. 27 for the period October 1, 1995 to September 30, 1996
- Optimization with variable-fidelity models applied to wing design
- PROFILE : airfoil geometry manipulation and display : user's guide
- Potential flow around two-dimensional airfoils using a singular integral method
- Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap
- Prediction of ice shapes and their effect on airfoil performance
- Results for the hybrid laminar flow control experiment conducted in the NASA Langley 3-FT transonic pressure tunnel on a 7-ft chord model
- SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions
- Spatial and temporal adaptive procedures for the unsteady aerodynamic analysis of airfoils using unstructured meshes
- Suppression of dynamic stall with a leading-edge slat on a VR-7 airfoil
- Swept wing attachment line contamination fence
- TADS--a CFD-based turbomachinery analysis and design system with GUI : version 2.0--methods and results
- TRANSEP, a program for high lift separated flow about airfoils
- Tables for correcting airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel for sidewall boundary layer effects
- Tables of properties of airfoil polynomials
- The paths of soaring flight
- The paths of soaring flight
- The structure of separated flow regions occuring near the leading edge of airfoils including transition
- The structure of separated flow regions occurring near the leading edge of airfoils, including transition : semi-annual status report, November 1984 - April 1985
- Two experimental supercritical laminar-flow-control swept-wing airfoils
- Two-dimensional aerodynamic characteristics of the Ames HI-120, HI-8, and LOW-12 airfoils
- Two-dimensional high-lift aerodynamic optimization using neural networks
- Verification of performance results for a low-speed 15% eliptical circulation control airfoil
- Wind tunnel aerodynamic characteristics of a transport-type airfoil in a simulated heavy rain environment
- Wing theory
- Wing theory
- [Life prediction and constitutive models for engine hot section anisotropic materials program] : [interim report]
- [Solution of separated flows using a simultaneous iteration technique] : [final report]

## Embed

### Settings

Select options that apply then copy and paste the RDF/HTML data fragment to include in your application

Embed this data in a secure (HTTPS) page:

Layout options:

Include data citation:

<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/WhMY6_tr3V8/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/WhMY6_tr3V8/">Aerofoils</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>

Note: Adjust the width and height settings defined in the RDF/HTML code fragment to best match your requirements

### Preview

## Cite Data - Experimental

### Data Citation of the Concept Aerofoils

Copy and paste the following RDF/HTML data fragment to cite this resource

`<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/WhMY6_tr3V8/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/WhMY6_tr3V8/">Aerofoils</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>`