#
Airfoils
Resource Information
The concept ** Airfoils** represents the subject, aboutness, idea or notion of resources found in **Houston Public Library**.

The Resource
Airfoils
Resource Information

The concept

**Airfoils**represents the subject, aboutness, idea or notion of resources found in**Houston Public Library**.- Label
- Airfoils

- Source
- nasat

## Context

Context of Airfoils#### Subject of

- 1987 Ground Vortex Workshop : proceedings of a meeting held at NASA Ames Research Center, Moffett Field, California, April 22-23, 1987
- 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
- A Modified lifted line theory for wing-propeller interference : progress report for the period June 1 to September 30, 1983
- A Two element laminar flow airfoil optimized for cruise
- A comparison of computer-generated lift and drag polars for a Wortman airfoil to flight and wind tunnel results : final report
- A comparison of design variables for control theory based airfoil optimization
- A computer program for estimating the areodynamic characteristics of NACA 16-series airfoils
- A computionally efficient modelling of laminar separation bubbles : semi-annual status report, June 1988 - January 1989 for NASA grant NAG-1-778
- A cooperative program to stimulate student involvement through the MIT undergraduate research opportunity program : final report
- A direct-inverse method for transonic and separated flows about airfoils
- A far-field non-reflecting boundary condition for two-dimensional wake flows
- A fully vectorized numerical solution of the incompressible Navier-Stokes equations
- A fundamental study of the sticking of insect residues to aircraft wings : annual technical report
- A laser-based ice shape profilometer for use in icing wind tunnels
- A lifting surface theory in rotational flow
- A recontoured, upper surface designed to increase the maximum lift coefficient of a modified NACA 65 (0.82) (9.9) airfoil section
- A simplified fourwall interference assessment procedure for airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel
- A steadying effect of acoustic excitation on transitory stall
- A viscous-inviscid interactive procedure for rotational flow in cascades of two dimensional airfoils of arbitrary shape : final report
- A wind tunnel study of icing effects on a business jet airfoil
- ALESEP, Part II : a computer program for the analysis of leading edge separation bubbles on infinite swept wings
- Acoustic scattering from ellipses by the modal element method
- Active control of flow separation over an airfoil
- Advanced ice protection systems test in the NASA Lewis Icing Research Tunnel
- 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 data banks for Clark-Y, NACA 4-digit, and NACA 16-series airfoil families
- 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
- Aerothermal modeling : phase 1 - final report : executive summary
- Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
- Airloads on bluff bodies, with application to the rotor-induced downloads on tilt-rotor aircraft
- An airfoil flutter model suspension system to accomdate large static transonic airloads
- An airfoil flutter model suspension system to accomdate 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 documentation of trailing-edge flows at high Reynolds number
- An experimental investigation of the confluent boundary layer on a high-lift system : final project report
- An experimental investigation of two 15%-scale wind tunnel fan-blade designs
- An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages
- An experimental low Reynolds number comparison of a Wortmann FX67-K170 airfoil, a NACA 0012 airfoil, and a NACA 64-210 airfoil in simulated heavy rain : final report to the NASA Langley Research Center on work accomplished under research grant NAG-1-568
- An experimental study of airfoil-spoiler aerodynamics
- An experimental study of airfoil-spoiler aerodynamics
- An experimental study of the aerodynamics of a NACA 0012 airfoil with a simulated glaze ice accretion
- An experimental study of the aerodynamics of a NACA0012 airfoil with a simulated glaze ice accretion, Volume II
- An exploratory investigation of a slotted, natural-laminar-flow airfoil
- An improved viscid/inviscid interaction procedure for transonic flow over airfoils
- An incremental strategy for calculating consistent discrete CFD sensitivity derivatives
- An integrated optimum design approach for high speed prop rotors : final report on NASA Ames grant no. NCC2-795
- Analysis of two-dimensional incompressible flow past airfoils using unsteady Navier-Stokes equations
- Annual progress report ... entitled "an experimental investigation of the flow physics of high-lift systems" for the period March-December 1995
- 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 transonic flow in a linear cascade
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- 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
- Control of separated flow past a cylinder using tangential wall jet blowing
- Control of unsteady separated flow associated with the dynamic stall of airfoils
- Control theory based airfoil design for potential flow and a finite volume discretization
- Control theory based airfoil design using the Euler equations
- Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel
- Corrections for attached sidewall boundary-layer effects in two-dimensional airfoil testing
- Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack : final report
- 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 fabrication of instrumented composite airfoils for a cryogenic wind tunnel model
- 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
- Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization : final report for the period ended September 30, 1995
- Droplet deformation prediction with the Droplet Deformation and Breakup Model (DDB)
- Effect of a rotor wake on heat transfer from a circular cylinder
- Effect of a rotor wake on the local heat transfer on the forward half of a circular cylinder
- Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing
- 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 environmentally imposed roughness on airfoil performance
- Effects of suction on swept-wing transition : final technical report on NASA-Langley award # NAG-1-194, 16 December 1995 to 31 March 1998
- Euler solutions using an implicit multigrid technique
- Evaluation of constant-Weber-number scaling for icing tests
- Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Experimental analyses of trailing edge flows : final technical report to NASA Ames Research Center
- 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
- Experimental study of complex vortex interactions in the wake of high aspect ratio wings : final report on NASA grant NAG-1-1816
- Feasability of predicting performance degradation of airfoils in heavy rain
- Final report for the period January 1, 1974 through December 31, 1983 entitled : Numerical solution of the Navier-Stokes equations for arbitrary two-dimensional multi-element airfoils
- 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
- Flow instabilities in transonic small disturbance theory
- Flow simulations about steady-complex and unsteady moving configurations using structured-overlapped and unstructured grids : abstract
- 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
- Further evaluation of traditional icing scaling methods
- Further investigations of icing effects on an advanced high-lift multi-element airfoil
- GRUMFOIL, a computer code for the viscous transonic flow over airfoils
- Global artificial boundary conditions for computation of external flow problems with propulsive jets
- Heat transfer in aeropropulsion systems
- Helicopter tail rotor noise analyses : final technical report ; period, June 1, 1985 - January 31, 1986
- High temperature thermocouple and heat flux gauge using a unique thin film-hardware hot junction
- ICEG2D (v2.0) : an integrated software package for automated prediction of flow fields for single-element airfoils with ice accretion
- Ice accretion with varying surface tension
- 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
- Icing simulation : a survey of computer models and experimental facilities
- Image processing of aerodynamic data
- 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
- 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
- Interactive aircraft flight control and aeroelastic stabilization : semi-annual report 1 November 1984 through 30 April 1985
- Inverse transonic airfoil design methods including boundary layer and viscous interaction effects : semiannual progress report, September 1, 1983 -- January 31, 1984
- 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
- MATE program : erosion resistant compressor airfoil coating, Volume II
- 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 approach for the aerodynamic analysis of airfoils with laminar separation
- Numerical simulation of the SOFIA flowfield
- 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
- On the flow processes in sharply inclined and stalled airfoils in parallel movement and rotation
- 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
- Optimization with variable-fidelity models applied to wing design
- Optimum aerodynamic design via boundary control
- Optimum transonic airfoils based on the Euler equations
- Potential flow analysis of glaze ice accretions on an airfoil
- 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 film cooling on gas turbine airfoils
- 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
- 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
- R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
- Rapport d'essais du profil CAST 10 en transition dĘąeclenchĘąee, effectuĘąes dans la soufflerie transsonique cryogĘąenique T2 en pr'esence de parois auto-adaptables : Report on tests of a CAST 10 airfoil with fiexed transition in the T2 transonic cryogenic wind tunnel with self-adaptive walls
- Results of S5 CH tests with an ARL (Aerospace Research Laboratory) cascade
- 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
- Semiempirical method for predicting vortex-induced rolling moments
- Shape Changing Airfoil
- SiC/SiC leading edge turbine airfoil tested under simulated gas turbine conditions
- Sidewall boundary-layer effects in two-dimensional airfoil testing : progress report for the period ending June 1985
- Simulation of self-induced unsteady motion in the near wake of a Joukowski airfoil
- 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
- Structural tailoring of engine blades (STAEBL), theoretical manual
- Structural tailoring of engine blades (STAEBL), user's manual
- Study of large-scale mixing in developing wakes behind streamlined bodies : final technical report
- Study of the TRAC airfoil table computational system
- Synthesized airfoil data method for predicttion of dynamic stall and unsteady airloads
- TADS, a CFD-based turbomachinery and analysis design system with GUI
- TADS--a CFD-based turbomachinery analysis and design system with GUI : version 2.0--methods and results
- Tabulation of data from tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- Tests of a NACA 651-213 airfoil in the NASA Langley 0.3 meter transonic cryogenic tunnel
- Tests on a CAST 7 two-dimensional airfoil in a self-streamlining test section
- The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis
- The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers
- The boundary layer on compressor cascade blades
- The boundary layer on compressor cascade blades
- The decay of longitudinal vortices shed from airfoil vortex generators
- The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model : final report
- The effects of the critical ice accretion on airfoil and wing performance : NASA contract # NCC3-408 : January 24, 1995-November 30, 1996 : final report
- The influence of free-stream turbulence on separation of turbulent boundary layers in incompressible, two-dimensional flow : final report
- The semi-discrete Galerkin finite element modelling of compressible viscous flow past an airfoil : final technical report
- The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel
- The structure of separated flow regions occurring near the leading edge of airfoils, including transition : semi-annual status report, February 1986-July 1986
- Thermal barrier coating life prediction model development : first annual report
- Thermal barrier coating life-prediction model development : second annual report
- Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis : abstract
- Three-dimensional unsteady lifting surface theory in the subsonic range
- Trailing edge flow conditions as a factor in airfoil design
- Trandesnf : a computer program for transonic airfoil design and analysis in nonuniform flow
- 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 calculation of airfoil stability and response with active controls
- Transonic interference reduction by limited ventilation wall panels
- 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
- Unsteady cascade aerodynamic response using a multiphysics simulation code
- Unsteady cascade aerodynamic response using a multiphysics simulation code
- User's manual for the NASA Lewis ice accretion/heat transfer prediction code with electrothermal deicer input
- Viscous effects on transonic airfoil stability and response
- Wing-section optimization for supersonic viscous flow : [abstract]
- Wing-section optimization for supersonic viscous flows : abstract

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