NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Advanced Technology Airfoil Research, volume 1, part 1A comprehensive review of all NASA airfoil research, conducted both in-house and under grant and contract, as well as a broad spectrum of airfoil research outside of NASA is presented. Emphasis is placed on the development of computational aerodynamic codes for airfoil analysis and design, the development of experimental facilities and test techniques, and all types of airfoil applications.
Document ID
19790011859
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
September 3, 2013
Publication Date
January 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-CP-2045-PT-1
L-12232-VOL-1-PT-1
Accession Number
79N20030
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19790011864WorkApplication of direct-inverse techniques to airfoil analysis and design19790011869WorkUpgraded viscous flow analysis of multi-element airfoils19790011870WorkNumerical solution of the Navier-Stokes equations for arbitrary two-dimensional multi-element airfoils19790011875WorkA study of the interaction of a normal shock wave with a turbulent boundary layer at transonic speeds19790011865WorkLow speed airfoil design and analysis19790011862WorkOverview of two-dimensional airfoil research at Ames Research Center19790011880WorkThe prediction of two-dimensional airfoil stall progression19790011878WorkApplication of numerical optimization to the design of advanced supercritical airfoils19790011881WorkApplication of the AMI C sub l sub max prediction method to a number of airfoils19790011874WorkWake curvature and trailing edge interaction effects in viscous flow over airfoils19790011877WorkSupercritical tests of a self-optimizing, variable-Camber wind tunnel model19790011866WorkA consistent design procedure for supercritical airfoils in free air and a wind tunnel19790011868WorkAn evaluation of four single element airfoil analytic methods19790011883WorkInverse boundary-layer technique for airfoil design19790011876WorkRecent developments in finite element analysis for transonic airfoils19790011884WorkLangley's two-dimensional research facilities: Capabilities and plans19790011888WorkSome steady and oscillating airfoil test results, including the effects of sweep, from the tunnel spanning wing19790011873WorkOptimization of multi-element airfoils for maximum lift19790011863WorkTransonic airfoil codes19790011860WorkNASA research objectives and roles19790011872WorkImprovements in surface singularity analysis and design methods19790011882WorkA new flow model for highly separated airfoil flows at low speeds19790011886WorkA new airfoil research capability19790011861WorkLangley airfoil-research program19790011887WorkDesign and calibration of slotted walls for transonic airfoil wind tunnels19790011879WorkImproved prediction of laminar leading edge separation19790011885WorkDevelopments in testing airfoil techniques at University of Southampton19790011867WorkProspects for computing airfoil aerodynamics with Reynolds averaged Navier-Stokes codes19790011871WorkThe analysis and design of transonic two-element airfoil systems
No Preview Available