NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Advanced technology airfoil research, volume 1, part 2This compilation contains papers presented at the NASA Conference on Advanced Technology Airfoil Research held at Langley Research Center on March 7-9, 1978, which have unlimited distribution. This conference provided a comprehensive review of all NASA airfoil research, conducted in-house and under grant and contract. A broad spectrum of airfoil research outside of NASA was also reviewed. The major thrust of the technical sessions were in three areas: development of computational aerodynamic codes for airfoil analysis and design, development of experimental facilities and test techniques, and all types of airfoil applications.
Document ID
19790011818
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Aeronautics (General)
Report/Patent Number
L-12232-VOL-1-PT-2
NASA-CP-2045-PT-2
Accession Number
79N19989
Funding Number(s)
PROJECT: RTOP 505-06-33-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19790011819WorkA parametric experimental study of the slotted-wall boundary condition19790011820WorkTransonic assessment of two-dimensional wind tunnel wall interference using measured wall pressures19790011821WorkResearch on self-correcting wind tunnels19790011822WorkAnalytical design of a contoured wind-tunnel liner for supercritical testing19790011823WorkEvaluation of interference in the OSU 6 in. by 22 in. transonic airfoil tunnel19790011824WorkVisualization of the separation and subsequent transition near the leading edge of airfoils19790011825WorkInstrumentation, techniques and data reduction associated with airfoil testing programs at Wichita State University19790011826WorkApplication of the laser velocimeter to airfoil research19790011827WorkApplications of dynamic measurement techniques to wind-tunnel testing19790011828WorkHolography and LDV techniques, their status and use in airfoil research19790011829WorkSection drag coefficients from pressure probe transverses of a wing wake at low speeds19790011830WorkFlight test techniques for low speed airfoil evaluation19790011831WorkIn-flight three-dimensional boundary layer and wake measurements from a swept supercritical wing19790011832WorkA procedure for analyzing transonic flow over harmonically oscillating airfoils19790011833WorkA new two-dimensional oscillating wing apparatus for unsteady aerodynamics research19790011834WorkSome calculations of transonic potential flow for the NACA 64A006 airfoil with oscillating flap19790011835WorkObservations on the dynamic stall characteristics of advanced helicopter rotor airfoils19790011836WorkTransonic flow over the NACA 64A006 with an oscillating flap-calculations based on the Euler equations
No Preview Available