Two experimental supercritical laminar-flow-control swept-wing airfoils View on Open Library

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

by Dennis O. Allison

No reviews yet
First published: 1987 1 language
Subjects
Transonic wind tunnels Sweptback wings Laminar flow airfoils Supercritical airfoils Wind tunnel tests Aerofoils

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by Dennis O. Allison

Assessment of dual-point drag reduction for an executive-jet modified airfoil section

Assessment of dual-point drag reduction ...

Calculation of thermodynamic properties of arbitrary gas mixtures with modified vibrational-rotational corrections

Calculation of thermodynamic properties ...

Semiempirical method for predicting vortex-induced rolling moments

Semiempirical method for predicting vort...

Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane

Airfoil modification effects on subsonic...

Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section

Aerodynamic characteristics and pressure...

Inviscid analysis of two supercritical laminar-flow-control airfoils at design and off-design conditions

Inviscid analysis of two supercritical l...

You Might Also Like

More in Transonic wind tunne...
Two-dimensional converging-diverging rippled nozzles at transonic speeds

Two-dimensional converging-diverging rip...

John R. Carlson
Slotted-wall flow-field measurements in a transonic wind tunnel

Slotted-wall flow-field measurements in ...

Joel L. Everhart
Assessment of dual-point drag reduction for an executive-jet modified airfoil section

Assessment of dual-point drag reduction ...

Dennis O. Allison
The NASA Langley 8-foot transonic pressure tunnel calibration

The NASA Langley 8-foot transonic pressu...

Cuyler W. Brooks
NASA Lewis 8- by 6-foot supersonic wind tunnel user manual

NASA Lewis 8- by 6-foot supersonic wind ...

Ronald H. Soeder
Control of the NASA Langley 16-foot transonic tunnel with the self-organizing feature map

Control of the NASA Langley 16-foot tran...

Mark A. Motter