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

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

by Charles D. Harris

No reviews yet
First published: 1988
Subjects
Boundary layer control Laminar boundary layer Supercritical wings Transonic flow

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by Charles D. Harris

Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel

Two-dimensional aerodynamic characterist...

The divine gift

The divine gift

God is alive and well

God is alive and well

Heaven? Yes! Hell? No!

Heaven? Yes! Hell? No!

NASA supercritical airfoils: a matrix of family-related airfoils

NASA supercritical airfoils: a matrix of...

Aerodynamic characteristics of the 10-percent-thick NASA supercritical airfoil 33 designed for a normal-force coefficient of 0.7

Aerodynamic characteristics of the 10-pe...

You Might Also Like

More in Boundary layer contr...
The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil

The NASA Langley laminar-flow-control ex...

Cuyler W. Brooks
Numerical simulation of the SOFIA flowfield

Numerical simulation of the SOFIA flowfi...

Stephen P. Klotz
Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control

Three-dimensional boundary-layer program...

Venkit Iyer
F-16XL-2 supersonic laminar flow control flight test experiment

F-16XL-2 supersonic laminar flow control...

Scott G. Anders
The boundary layer on compressor cascade blades

The boundary layer on compressor cascade...

Steven Deutsch
Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system

Simulated-airline-service flight tests o...

Dal V. Maddalon