Author: J. J. Olsen
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 218
Book Description
The report presents and interprets the predictions of an unsteady aerodynamic prediction method known as the Sonic Box method. Illustrations are given on how the program interprets input modal data, the program's techniques for smoothing certain input and output data, convergence of the numerical results, and comparisons of predicted results with experiments. It is shown how the present program requires the user to devote some care to defining input mode shapes, however this problem can be removed by a simple modification. Generally speaking, the program's current limit of fifty boxes in any one direction is sufficient to obtain satisfactory convergence, with the exception of pitching moments on cropped deltas. In this respect other modifications are apparent which could improve convergence at the cost of increased complexity. Agreement with experiment was generally qualitatively good, but illustrated the need for further optimization of the method as well as the lack of experimental data of the type and quality desired for correlation. (Author).
Demonstration of a Transonic Box Method for Unsteady Aerodynamics of Planar Wings
Author: J. J. Olsen
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 218
Book Description
The report presents and interprets the predictions of an unsteady aerodynamic prediction method known as the Sonic Box method. Illustrations are given on how the program interprets input modal data, the program's techniques for smoothing certain input and output data, convergence of the numerical results, and comparisons of predicted results with experiments. It is shown how the present program requires the user to devote some care to defining input mode shapes, however this problem can be removed by a simple modification. Generally speaking, the program's current limit of fifty boxes in any one direction is sufficient to obtain satisfactory convergence, with the exception of pitching moments on cropped deltas. In this respect other modifications are apparent which could improve convergence at the cost of increased complexity. Agreement with experiment was generally qualitatively good, but illustrated the need for further optimization of the method as well as the lack of experimental data of the type and quality desired for correlation. (Author).
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 218
Book Description
The report presents and interprets the predictions of an unsteady aerodynamic prediction method known as the Sonic Box method. Illustrations are given on how the program interprets input modal data, the program's techniques for smoothing certain input and output data, convergence of the numerical results, and comparisons of predicted results with experiments. It is shown how the present program requires the user to devote some care to defining input mode shapes, however this problem can be removed by a simple modification. Generally speaking, the program's current limit of fifty boxes in any one direction is sufficient to obtain satisfactory convergence, with the exception of pitching moments on cropped deltas. In this respect other modifications are apparent which could improve convergence at the cost of increased complexity. Agreement with experiment was generally qualitatively good, but illustrated the need for further optimization of the method as well as the lack of experimental data of the type and quality desired for correlation. (Author).
Unsteady Aerodynamics
Author: Grigorios Dimitriadis
Publisher: John Wiley & Sons
ISBN: 1119762472
Category : Technology & Engineering
Languages : en
Pages : 581
Book Description
Unsteady Aerodynamics A comprehensive overview of unsteady aerodynamics and its applications The study of unsteady aerodynamics goes back a century and has only become more significant as aircraft become increasingly sophisticated, fly faster, and their structures are lighter and more flexible. Progress in the understanding of flow physics, computing power and techniques, and modelling technologies has led to corresponding progress in unsteady aerodynamics, with a wide range of methods currently used to predict the performance of engineering structures under unsteady conditions. Unsteady Aerodynamics offers a comprehensive and systematic overview of the application of potential and vortex methods to the subject. Beginning with an introduction to the fundamentals of unsteady flow, it then discusses the modelling of attached and separated, incompressible and compressible flows around two-dimensional and three-dimensional bodies. The result is an essential resource for design and simulation in aerospace engineering. Unsteady Aerodynamics readers will also find: MATLAB examples and exercises throughout, with codes and solutions on an accompanying website Detailed discussion of most classes of unsteady phenomena, including flapping flight, transonic flow, dynamic stall, flow around bluff bodies and more Validation of theoretical and numerical predictions using comparisons to experimental data from the literature Unsteady Aerodynamics is ideal for researchers, engineers, and advanced students in aerospace engineering.
Publisher: John Wiley & Sons
ISBN: 1119762472
Category : Technology & Engineering
Languages : en
Pages : 581
Book Description
Unsteady Aerodynamics A comprehensive overview of unsteady aerodynamics and its applications The study of unsteady aerodynamics goes back a century and has only become more significant as aircraft become increasingly sophisticated, fly faster, and their structures are lighter and more flexible. Progress in the understanding of flow physics, computing power and techniques, and modelling technologies has led to corresponding progress in unsteady aerodynamics, with a wide range of methods currently used to predict the performance of engineering structures under unsteady conditions. Unsteady Aerodynamics offers a comprehensive and systematic overview of the application of potential and vortex methods to the subject. Beginning with an introduction to the fundamentals of unsteady flow, it then discusses the modelling of attached and separated, incompressible and compressible flows around two-dimensional and three-dimensional bodies. The result is an essential resource for design and simulation in aerospace engineering. Unsteady Aerodynamics readers will also find: MATLAB examples and exercises throughout, with codes and solutions on an accompanying website Detailed discussion of most classes of unsteady phenomena, including flapping flight, transonic flow, dynamic stall, flow around bluff bodies and more Validation of theoretical and numerical predictions using comparisons to experimental data from the literature Unsteady Aerodynamics is ideal for researchers, engineers, and advanced students in aerospace engineering.
Performance and Dynamics of Aerospace Vehicles
Author: Langley Research Center
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 694
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 694
Book Description
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Book Description
A Compilation of Computer Programs in Flight Vehicle Technology
Author: Ambrose B. Nutt
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 164
Book Description
A compilation of computer programs useful in the design of flight vehicles. Technical domains covered include the following: Structures; Aerodynamics; Vehicle dynamics; Flight control; Environmental control; Crew escape and retardation; and Landing gear subsystems. All programs were devised in-house in the Air Force Flight Dynamics Laboratory or were prepared for them under R and D contracts. (Author).
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 164
Book Description
A compilation of computer programs useful in the design of flight vehicles. Technical domains covered include the following: Structures; Aerodynamics; Vehicle dynamics; Flight control; Environmental control; Crew escape and retardation; and Landing gear subsystems. All programs were devised in-house in the Air Force Flight Dynamics Laboratory or were prepared for them under R and D contracts. (Author).
AIAA Dynamics Specialists Conference
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 292
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 292
Book Description
U. S. Government Research and Development Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1776
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1776
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
Book Description
AIAA Journal
Author: American Institute of Aeronautics and Astronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1024
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1024
Book Description
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 908
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 908
Book Description