Survey of experimental data of selected supercritical airfoils

Schiktanz, Daniel; Scholz, Dieter

doi:10.48441/4427.2478

Please use this identifier to cite or link to this item: https://doi.org/10.48441/4427.2478

Publisher URL:	https://www.fzt.haw-hamburg.de/pers/Scholz/Airport2030/Airport2030_TN_Supercritical_Airfoils_11-12-21.pdf
Title:	Survey of experimental data of selected supercritical airfoils
Language:	English
Authors:	Schiktanz, Daniel Scholz, Dieter
Keywords:	aviation; airliners; commercial; aircraft; design; wing; airfoil; catalog; supercritical; aerodynamics; wind tunnel; test; NASA; Langley; transonic; relative; thickness; lift; coefficient; Mach; Reynolds; number
Issue Date:	21-Dec-2011
Project:	Spitzencluster Luftfahrt - Metropolregion Hamburg; Teilprojekt 3: Effizienter Flughafen 2030
Abstract:	This survey was prepared for having a structured compendium about the aerodynamic characteristics of several supercritical airfoils. It may be used within the scope of the design of commercial airliners. The survey is based on published data coming from wind tunnel tests performed at the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel. All of the referenced reports are published on the NASA Technical Reports Server (NTRS).
URI:	https://hdl.handle.net/20.500.12738/17594
DOI:	10.48441/4427.2478
Review status:	Currently there is no review planned for this version
Institute:	Forschungsgruppe Flugzeugentwurf und -systeme (AERO) Department Fahrzeugtechnik und Flugzeugbau Fakultät Technik und Informatik
Type:	Report
Additional note:	SCHIKTANZ, Daniel, SCHOLZ, Dieter, 2011. Survey of Experimental Data of Selected Supercritical Airfoils. Technical Note. Aircraft Design and Systems Group (AERO). Hamburg University of Applied Sciences (HAW Hamburg). Available from: https://doi.org/10.48441/4427.2478
Funded by:	Bundesministerium für Forschung, Technologie und Raumfahrt
Appears in Collections:	Publications with full text