Flow Visualization of a Rolling Delta Wing and Its Pertinence to the Non-linear Indicial Response Model

Flow Visualization of a Rolling Delta Wing and Its Pertinence to the Non-linear Indicial Response Model PDF Author: Gregory Addington
Publisher:
ISBN:
Category :
Languages : en
Pages :

Get Book Here

Book Description

Flow Visualization of a Rolling Delta Wing and Its Pertinence to the Non-linear Indicial Response Model

Flow Visualization of a Rolling Delta Wing and Its Pertinence to the Non-linear Indicial Response Model PDF Author: Gregory Addington
Publisher:
ISBN:
Category :
Languages : en
Pages :

Get Book Here

Book Description


Journal of Aircraft

Journal of Aircraft PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 492

Get Book Here

Book Description


AIAA Flight Simulation Technologies Conference

AIAA Flight Simulation Technologies Conference PDF Author:
Publisher:
ISBN:
Category : Flight simulators
Languages : en
Pages : 478

Get Book Here

Book Description


Motion Effects on Leading-Edge Vortex Behavior Over Delta Wings and Generalized Modeling

Motion Effects on Leading-Edge Vortex Behavior Over Delta Wings and Generalized Modeling PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 23

Get Book Here

Book Description


Aerospace America

Aerospace America PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 634

Get Book Here

Book Description


Conical Euler Analysis and Active Roll Suppression for Unsteady Vortical Flows about Rolling Delta Wings

Conical Euler Analysis and Active Roll Suppression for Unsteady Vortical Flows about Rolling Delta Wings PDF Author: Elizabeth M. Lee-Rausch
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36

Get Book Here

Book Description


Computation of a Delta-wing Roll-and-hold Maneuver

Computation of a Delta-wing Roll-and-hold Maneuver PDF Author: Raymond E. Gordnier
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 50

Get Book Here

Book Description
This report presents computations of the flowfield around an 80 degree sweep delta wing undergoing a constant roll-rate maneuver from 0 to 45 degrees. The governing equations for the problem are the unsteady, three- dimensional Navier-Stokes equations. The equations are solved using the implicit, approximately-factored algorithm of Beam-Warming. Fixed roll angle results are also presented and compared with experimental measurements to demonstrate the ability of the numerical technique to accurately capture the flowfield around a rolled delta wing. The dynamic behaviors of the vortex position and strength, as well as their corresponding effect on surface pressure, lift and roll moment, are described. A simple, quasi-static explanation of these vortex behaviors based on effective angle-of-attack and sideslip angle is proposed ... Delta wing roll, Vortex dynamics, Vortical flow, Unsteady maneuver.

Flow Visualization Image Analysis of High-rate Roll Experiments on a Delta Wing

Flow Visualization Image Analysis of High-rate Roll Experiments on a Delta Wing PDF Author: Eric J. Stephen
Publisher:
ISBN:
Category :
Languages : en
Pages :

Get Book Here

Book Description


Thrust-induced Effects on a Pitching-up Delta Wing Flow Field

Thrust-induced Effects on a Pitching-up Delta Wing Flow Field PDF Author: Leon L. Van Dommelen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 30

Get Book Here

Book Description
Neural network procedures were explored with the objectives to control a delta wing in the non-linear domain. Results show that neural networks are well suited to represent non-linear computed lift and pressure forces on delta wings. A model problem, the flare maneuver, suggests that neural network controllers can perform well for non-linear systems provided that suitable input and training data are provided to it.

Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model

Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model PDF Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Vibration
Languages : en
Pages : 54

Get Book Here

Book Description