Supercritical Airfoils

25 books
NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnelRenaldo V. Jenkins
⏱ 55m

NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel

Renaldo V. Jenkins

198955 pp.
Windkanaluntersuchungen an dunnen superkritischen Profilen im hohen UnterschallHorst Korner

Windkanaluntersuchungen an dunnen superkritischen Profilen im hohen Unterschall

Horst Korner

1982No page data
NASA supercritical airfoils: a matrix of family-related airfoilsCharles D. Harris
⏱ 1h 11m

NASA supercritical airfoils: a matrix of family-related airfoils

Charles D. Harris

199071 pp.
Unsteady aerodynamics of conventional and supercritical airfoilsSanford S. Davis
⏱ 7h 13m

Unsteady aerodynamics of conventional and supercritical airfoils

Sanford S. Davis

1980433 pp.
Computational and experimental research on buffet phenomena of transonic airfoilsNaoki Hirose
⏱ 20m

Computational and experimental research on buffet phenomena of transonic airfoils

Naoki Hirose

198820 pp.
A direct-inverse method for transonic and separated flows about airfoilsLeland A. Carlson
⏱ 1h 8m

A direct-inverse method for transonic and separated flows about airfoils

Leland A. Carlson

199068 pp.
The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoilCuyler W. Brooks
⏱ 18m

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil

Cuyler W. Brooks

198918 pp.
Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wingDavid A. Seidel
⏱ 5h 12m

Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing

David A. Seidel

1991312 pp.
Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speedsY. Y. Chan
⏱ 31m

Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds

Y. Y. Chan

198831 pp.
Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-Meter Transonic Cryogenic TunnelRenaldo Jenkins
⏱ 4h 56m

Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-Meter Transonic Cryogenic Tunnel

Renaldo Jenkins

1988296 pp.
Two-dimensional wind-tunnel tests of a NASA supercritical airfoil with various high-lift systems. Volume 1: Data analysisE. Omar
⏱ 1h 24m

Two-dimensional wind-tunnel tests of a NASA supercritical airfoil with various high-lift systems. Volume 1: Data analysis

E. Omar

197784 pp.
Influence of the transonic doublet in the farfield of a lifting airfoilM. Mokry
⏱ 18m

Influence of the transonic doublet in the farfield of a lifting airfoil

M. Mokry

199318 pp.
Revised results of the unsteady transonic pressure measurements on the LANN modelR. G. den Boer
⏱ 2h 36m

Revised results of the unsteady transonic pressure measurements on the LANN model

R. G. den Boer

1989156 pp.
Blunt trailing edge analysis of supercritical airfoils by a Navier-Stokes codeNaoki Hirose
⏱ 24m

Blunt trailing edge analysis of supercritical airfoils by a Navier-Stokes code

Naoki Hirose

199024 pp.
Control of unsteady separated flow associated with the dynamic stall of airfoilsMichael C. Wilder

Control of unsteady separated flow associated with the dynamic stall of airfoils

Michael C. Wilder

1992No page data
Two experimental supercritical laminar-flow-control swept-wing airfoilsDennis O. Allison
⏱ 22m

Two experimental supercritical laminar-flow-control swept-wing airfoils

Dennis O. Allison

198722 pp.
Flow and turbulence modeling and computation of shock buffet onset for conventional and supercritical airfoilsRobert E. Bartels

Flow and turbulence modeling and computation of shock buffet onset for conventional and supercritical airfoils

Robert E. Bartels

1998No page data
Comparison of computational and experimental results for a supercritical airfoilMelissa B. Rivers

Comparison of computational and experimental results for a supercritical airfoil

Melissa B. Rivers

1994No page data
Three-dimensional aerodynamic shape optimization using discrete sensitivity analysisGregory Wayne Burgreen

Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis

Gregory Wayne Burgreen

1995No page data
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic TunnelWilliam G. Johnson

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

William G. Johnson

1985No page data
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