High-lift system aerodynamics View on Open Library

High-lift system aerodynamics

by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

No reviews yet
First published: 1993 1 language ISBN: 9283507150
Subjects
High lift systems

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Flight test techniques

Flight test techniques

Missile aerodynamics

Missile aerodynamics

Recent advances in aerothermochemistry

Recent advances in aerothermochemistry

Erosion, corrosion and foreign object damage effects in gas turbines

Erosion, corrosion and foreign object da...

Secondary flows in turbomachines

Secondary flows in turbomachines

A manual on the evaluation of information centers and services

A manual on the evaluation of informatio...

You Might Also Like

More in High lift systems
Additional flow field studies of the GA(W)-1 airfoil with 30-percent chord Fowler flap including slot-gap variations and cove shape modifications

Additional flow field studies of the GA(...

W. H. Wentz
Numerical analysis of multiple element high lift devices by Navier Stokes equation using implicit TVD finite volume method

Numerical analysis of multiple element h...

Eiji Shima
Force measurements on caret and delta wings at high incidence

Force measurements on caret and delta wi...

G. T. Colemann
High lift system aerodynamics: papers presented and discussions recorded at the 71st Fluid Dynamics Panel Meeting and at the Symposium held in Banff, Alberta, Canada, from 5th-8th October 1992

High lift system aerodynamics: papers pr...

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
High lift aerodynamics for transport aircraft by interactive experimental and theoretical tool development

High lift aerodynamics for transport air...

J. Szodruch
Aerodynamic characteristics of a propeller-powered high-lift semispan wing

Aerodynamic characteristics of a propell...

Garl L. Gentry