Amanote Research

Amanote Research

    RegisterSign In

Flight Mechanics Model for Spanwise Lift and Rolling Moment Distributions of a Segmented Active High-Lift Wing

CEAS Aeronautical Journal - United States
doi 10.1007/s13272-017-0261-4
Full Text
Open PDF
Abstract

Available in full text

Categories
TransportationAerospace Engineering
Date

September 20, 2017

Authors
J. H. DiekmannD. KellerE. FaezR. RudnikV. Gollnick
Publisher

Springer Science and Business Media LLC


Related search

Propeller and Active High Lift Wing Interaction in Experiment and Simulation

Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Transfer ProcessesFluid Flow
2016English

A Simple Approximation Method for Obtaining the Spanwise Lift Distribution

The Journal of the Royal Aeronautical Society
1941English

Unsteady Lift and Moment of a Periodically Plunging Airfoil

AIAA Journal
Aerospace Engineering
2019English

Active Flow Separation Control on a High-Lift Wing-Body Configuration Part 2: The Pulsed Blowing Application

2011English

Flight With Lift Modulation Inside a Planetary Atmosphere

AIAA Journal
Aerospace Engineering
1977English

High-Lift Aerodynamics

Journal of Aircraft
Aerospace Engineering
1975English

Total Facelift: Forehead Lift, Midface Lift, and Neck Lift

Archives of Plastic Surgery
Surgery
2015English

Didactic Model of Lift

TECHNICAL SCIENCES AND TECHNOLOG IES
2018English

Lift Enhancement of Delta Wing With Trailing Edge Jet

Journal of the Japan Society for Aeronautical and Space Sciences
2004English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy