Prediction of Wing Aeroelastic Effects on Aircraft Lift and Pitching Moment Characteristics

Prediction of Wing Aeroelastic Effects on Aircraft Lift and Pitching Moment Characteristics PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

Get Book Here

Book Description

Prediction of Wing Aeroelastic Effects on Aircraft Lift and Pitching Moment Characteristics

Prediction of Wing Aeroelastic Effects on Aircraft Lift and Pitching Moment Characteristics PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

Get Book Here

Book Description


Effects of Flexibility on Lift and Pitching-moment Characteristics of a Series of Low-aspect-ratio Wing-body Combinations at Transonic Speeds

Effects of Flexibility on Lift and Pitching-moment Characteristics of a Series of Low-aspect-ratio Wing-body Combinations at Transonic Speeds PDF Author: Robert V. Doggett
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58

Get Book Here

Book Description


Light Aircraft Lift, Drag, and Moment Prediction

Light Aircraft Lift, Drag, and Moment Prediction PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 500

Get Book Here

Book Description


Lift, Pitching Moment, and Span Load Characteristics of Wings at Low Speed as Affected by Variations of Sweep and Aspect Ratio

Lift, Pitching Moment, and Span Load Characteristics of Wings at Low Speed as Affected by Variations of Sweep and Aspect Ratio PDF Author: Edward J. Hopkins
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 40

Get Book Here

Book Description
Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0, 35, and 45 degrees. The wing span was decreased to give aspect ratios 6.8, 5.3, 4.2, 3.4, and 2.8. The effects of independent variations of sweep and aspect ratio on the lift, pitching-moment, and span-load characteristics of the wings are compared with the effects estimated by use of the Weissinger method.

An Analysis of the Effects of Aeroelasticity on Static Longitudinal Stability and Control of a Swept-back-wing Airplane

An Analysis of the Effects of Aeroelasticity on Static Longitudinal Stability and Control of a Swept-back-wing Airplane PDF Author: Richard B. Skoog
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 50

Get Book Here

Book Description


Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack

Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack PDF Author: James M. Luckring
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 104

Get Book Here

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460

Get Book Here

Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Investigation of Some Effects of Flexibility on the Lift and Pitching-moment Characteristics of a Series of Low-aspect- Ratio Wing-body Combinations at Transonic Speeds

Investigation of Some Effects of Flexibility on the Lift and Pitching-moment Characteristics of a Series of Low-aspect- Ratio Wing-body Combinations at Transonic Speeds PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54

Get Book Here

Book Description


An Analysis of Methods for Predicting the Stability Characteristics of an Elastic Airplane. Appendix B - Methods for Determining Stability Derivatives

An Analysis of Methods for Predicting the Stability Characteristics of an Elastic Airplane. Appendix B - Methods for Determining Stability Derivatives PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 674

Get Book Here

Book Description


Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63

Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63 PDF Author: Maurice O. Feryn
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

Get Book Here

Book Description