Trailing Edges Aerodynamics

13 books
Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap systemDaniel W. Banks
⏱ 1h 52m

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

Daniel W. Banks

1987112 pp.
High-lift systems on commercial subsonic airlinersPeter K. C. Rudolph
⏱ 2h 35m

High-lift systems on commercial subsonic airliners

Peter K. C. Rudolph

1996155 pp.
Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES programBruce Charles

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

Bruce Charles

1999No page data
Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanesUnited States.: National Advisory Committee for Aeronautics
⏱ 58m

Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes

United States.: National Advisory Committee for Aeronautics

194458 pp.
Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flapsHarold William Davidson
⏱ 1h 58m

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

Harold William Davidson

1951118 pp.
Trailing edge flow conditions as a factor in airfoil designA. I. Ormsbee

Trailing edge flow conditions as a factor in airfoil design

A. I. Ormsbee

1984No page data
Assessment of dual-point drag reduction for an executive-jet modified airfoil sectionDennis O. Allison
⏱ 1h 54m

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

Dennis O. Allison

1996114 pp.
Near field trailing edge tone noise computationChing Y. Loh

Near field trailing edge tone noise computation

Ching Y. Loh

2002No page data
Active Spanwise Lift ControlJoaquim Neto Dias

Active Spanwise Lift Control

Joaquim Neto Dias

2020No page data
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊Scott P. Fears
⏱ 2h 25m

Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊

Scott P. Fears

1995145 pp.
Predicting modes of the unsteady vorticity field near the trailing edge of a bladeWilliam J. Devenport

Predicting modes of the unsteady vorticity field near the trailing edge of a blade

William J. Devenport

2003No page data
Development of direct-inverse 3-D method for applied aerodynamic design and analysisLeland A. Carlson

Development of direct-inverse 3-D method for applied aerodynamic design and analysis

Leland A. Carlson

1987No page data
Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flapAhmed Hassan

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

Ahmed Hassan

1999No page data