Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap View on Open Library

Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap

by Ahmed Hassan

No reviews yet
First published: 1999 1 language
Subjects
Trailing edge flaps Computational grids Aerodynamic characteristics Blade-vortex interaction Grid generation (Mathematics) Airfoils Noise reduction Navier-Stokes equation

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by Ahmed Hassan

Advances in Model and Data Engineering in the Digitalization Era

Advances in Model and Data Engineering i...

My Photo Dictionary French-Arabic

My Photo Dictionary French-Arabic

Prophetic Biography

Prophetic Biography

Picture Dictionary English-Arabic

Picture Dictionary English-Arabic

Prophetic Biography Part Two

Prophetic Biography Part Two

Analysis of the Factors Responsible for the Alienation of Genderqueers in West Punjab Pakistan

Analysis of the Factors Responsible for ...

You Might Also Like

More in Trailing edge flaps
High-lift systems on commercial subsonic airliners

High-lift systems on commercial subsonic...

Peter K. C. Rudolph
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ĚŠ

Low-speed wind-tunnel investigation of t...

Scott P. Fears
Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system

Low-speed aerodynamic characteristics of...

Daniel W. Banks
Wing pressure distributions from subsonic tests of a high-wing transport model

Wing pressure distributions from subsoni...

Zachary T. Applin
Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program

Implementation of a trailing-edge flap a...

Bruce Charles
Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps

Lift increase obtained with boundary lay...

Harold William Davidson