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

The Resource
Airfoils
Resource Information

The concept

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

- Source
- nasat

## Context

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- Unsteady cascade aerodynamic response using a multiphysics simulation code
- A computer program for estimating the areodynamic characteristics of NACA 16-series airfoils
- A direct-inverse method for transonic and separated flows about airfoils
- A preconditioning method for shape optimization governed by the Euler equations
- A wind tunnel study of icing effects on a business jet airfoil
- Active control of flow separation over an airfoil
- Advanced turbine study : final report
- Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
- Aerodynamic classification of swept-wing ice accretion
- Aerodynamic classification of swept-wing ice accretion
- Aerodynamic design of a propeller for high-altitude balloon trajectory control
- Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation
- Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditions
- Aerodynamic simulation of ice accretion on airfoils
- Airloads on bluff bodies, with application to the rotor-induced downloads on tilt-rotor aircraft
- An airfoil flutter model suspension system to accommodate large static transonic airloads
- An approach to the constrained design of natural laminar flow airfoils
- An experimental and computational investigation of oscillating airfoil unsteady aerodynamics at large mean incidence
- An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages
- An experimental study of airfoil-spoiler aerodynamics
- An exploratory investigation of a slotted, natural-laminar-flow airfoil
- An incremental strategy for calculating consistent discrete CFD sensitivity derivatives
- Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques
- Artificial boundary conditions for computation of oscillating external flows
- Artificial boundary conditions for computation of oscillating external flows
- Assessment of two-equation turbulence models for transonic flows
- CFD study of NACA 0018 airfoil with flow control
- Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- Closed-loop separation control using oscillatory flow excitation
- Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
- Comparison of several dissipation algorithms for central difference schemes
- Compressible flows with periodic vortical disturbances around lifting airfoils
- Computational fluid mechanics : progress report no. 18
- Computer program to obtain ordinates for NACA airfoils
- Computer programs for smoothing and scaling airfoil coordinates
- Continued development and application of circulation control pneumatic technology to advanced transport aircraft : NASA grant NAG-1-1517 : period covered, June 14, 1993 to August 31, 1997
- Control of flow separation and mixing by aerodynamic excitation
- Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel
- Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions
- Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions
- DRA/NASA/ONERA collaboration on icing research, Part II, Prediction of airfoil ice accretion
- Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment
- Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment
- Design of a slotted, natural-laminar-flow airfoil for business-jet applications
- Development and testing of airfoils for high-altitude aircraft : final report
- Development, verification and use of gust modeling in the NASA computational fluid dynamics code FUN3D
- Distributed-roughness effects on stability and transition in swept-wing boundary layers : annual technical report ... NASA-Langley cooperative agreement # NCC-1-194 and the Boeing Company contract #ZA0078, during 5/17/96-12/31/96
- Droplet deformation prediction with the Droplet Deformation and Breakup Model (DDB)
- Effect of in-flight ice accretion on the performance of a multi-element airfoil
- Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
- Effects of suction on swept-wing transition : final technical report on NASA-Langley award # NAG-1-194, 16 December 1995 to 31 March 1998
- Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
- 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 investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet
- Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet
- Experimental observations on the deformation and breakup of water droplets near the leading edge of an airfoil
- Experimental optimization methods for multi-element airfoils : final report
- Experimental studies of low-pressure turbine flows and flow control : final report
- Final report on study of organized structures in the post-stall flow over wings
- Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
- Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
- Flow control under low-pressure turbine conditions using pulsed jets : final report
- Free-form airfoil shape optimization under uncertainty using maximum expected value and second-order second-moment strategies
- Fundamental ice crystal accretion physics studies
- Further evaluation of scaling methods for rotorcraft icing
- Global artificial boundary conditions for computation of external flow problems with propulsive jets
- ICEG2D (v2.0) : an integrated software package for automated prediction of flow fields for single-element airfoils with ice accretion
- Ice accretions and full-scale iced aerodynamic performance data for a two-dimensional NACA 23012 airfoil
- Ice accretions and icing effects for modern airfoils
- Icing encounter duration sensitivity study
- Implementation of advanced two equation turbulence models in the USM3D unstructured flow solver
- Impulsive start of a symmetric airfoil at high angle of attack
- In-flight measurements of wing ice shapes and wing section drag increases caused by natural icing conditions
- Key topics for high-lift research : a joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996
- Life prediction and constitutive models for engine hot section anisotropic materials program : annual status report
- Mechanism of water droplet breakup near the leading edge of an airfoil
- Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : final report for the period ended December 31, 1995
- Modern airfoil ice accretions
- Modern airfoil ice accretions
- Numerical solutions of the complete Navier-Stokes equations : progress report no. 27 for the period October 1, 1995 to September 30, 1996
- Numerical study of turbulence model predictions for the MD 30P/30N and NHLP-2D three-element highlift configurations
- On central-difference and upwind schemes
- Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel
- Optimization of an advanced design three-element airfoil at high Reynolds numbers
- Optimum transonic airfoils based on the Euler equations
- Potential flow analysis of glaze ice accretions on an airfoil
- Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight : final technical report under NASA-Ames research grant no. NAG 2-797
- Preliminary design of a supersonic cruise aircraft high-pressure turbine : final report
- R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
- Results of an experimental program investigating the effects of simulated ice on the performance of the NACA 63A415 airfoil with flap
- Robust airfoil optimization to achieve consistent drag reduction over a mach range
- Shape Changing Airfoil
- SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions
- Simulation of a controlled airfoil with jets
- SmaggIce 2.0 : additional capabilities for interactive grid generation of iced airfoils
- SmaggIce : surface modeling and grid generation for iced airfoils, phase I results
- SmaggIce user guide : SmaggIce version 1.0
- SmaggIce, surface modeling and grid generation for iced airfoils : phase 1 results
- Spanwise spacing effects on the initial structure and decay of axial vortices : under contract NAS3-27377
- Study of the TRAC airfoil table computational system
- Synthesized airfoil data method for predicttion of dynamic stall and unsteady airloads
- Tabulation of data from tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis
- The effects of the critical ice accretion on airfoil and wing performance : NASA contract # NCC3-408 : January 24, 1995-November 30, 1996 : final report
- Trailing edge flow conditions as a factor in airfoil design
- Transient growth theory prediction of optimal placing of passive and active flow control devices for separation delay in LPT airfoils
- Transonic airfoil analysis and design in nonuniform flow
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method : EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, GĂ¶ttingen, Germany, September 16-18, 1996
- Two-dimensional high-lift aerodynamic optimization using neural networks
- Unsteady cascade aerodynamic response using a multiphysics simulation code

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