Flutter at Very High Speeds

Flutter at Very High Speeds PDF Author: Harry L. Runyan
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 16

Book Description
This paper is concerned with a discussion of some of the problems of flutter and aeroelasticity that are or may be important at high speeds. Various theoretical procedures for treating high Mach number flutter are reviewed. Application of two of these methods, namely, the Van Dyke method and piston-theory method, is made to a specific example and compared with linear two- and three-dimensional results. It is shown that the effects of thickness and airfoil shape are destabilizing as compared with linear theory at high Mach number. In order to demonstrate the validity of these large predicted effects, experimental flutter results are shown for two rectangular wings at Mach numbers of 6.86 and 3. The results of nonlinear piston-theory calculations were in good agreement with experiment, whereas the results of using two- and three-dimensional linear theory were not. In addition, some results demonstrating the importance of including camber modes in a flutter analysis are shown, as well as a discussion of one case of flutter due to aerodynamic heating.

Flutter at Very High Speeds

Flutter at Very High Speeds PDF Author: Harry L. Runyan
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 16

Book Description
This paper is concerned with a discussion of some of the problems of flutter and aeroelasticity that are or may be important at high speeds. Various theoretical procedures for treating high Mach number flutter are reviewed. Application of two of these methods, namely, the Van Dyke method and piston-theory method, is made to a specific example and compared with linear two- and three-dimensional results. It is shown that the effects of thickness and airfoil shape are destabilizing as compared with linear theory at high Mach number. In order to demonstrate the validity of these large predicted effects, experimental flutter results are shown for two rectangular wings at Mach numbers of 6.86 and 3. The results of nonlinear piston-theory calculations were in good agreement with experiment, whereas the results of using two- and three-dimensional linear theory were not. In addition, some results demonstrating the importance of including camber modes in a flutter analysis are shown, as well as a discussion of one case of flutter due to aerodynamic heating.

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 498

Book Description


Aeroelastic Research at High Speeds

Aeroelastic Research at High Speeds PDF Author: A. Gerald Rainey
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

Book Description


Technical Data Digest

Technical Data Digest PDF Author:
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 770

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 536

Book Description


The Aeroplane

The Aeroplane PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 880

Book Description


Departments of State, Justice, and Commerce Appropriation Bill for 1937

Departments of State, Justice, and Commerce Appropriation Bill for 1937 PDF Author: United States. Congress. Senate. Committee on Appropriations
Publisher:
ISBN:
Category :
Languages : en
Pages : 1050

Book Description


Sound & Hearing

Sound & Hearing PDF Author: R. Duncan Luce
Publisher: Psychology Press
ISBN: 1317759796
Category : Language Arts & Disciplines
Languages : en
Pages : 394

Book Description
The major aim of this book is to introduce the ways in which scientists approach and think about a phenomenon -- hearing -- that intersects three quite different disciplines: the physics of sound sources and the propagation of sound through air and other materials, the anatomy and physiology of the transformation of the physical sound into neural activity in the brain, and the psychology of the perception we call hearing. Physics, biology, and psychology each play a role in understanding how and what we hear. The text evolved over the past decade in an attempt to convey something about scientific thinking, as evidenced in the domain of sounds and their perception, to students whose primary focus is not science. It does so using a minimum of mathematics (high school functions such as linear, logarithmic, sine, and power) without compromising scientific integrity. A significant enrichment is the availability of a compact disc (CD) containing over 20 examples of acoustic demonstrations referred to in the book. These demonstrations, which range from echo effects and filtered noise to categorical speech perception and total more than 45 minutes, are invaluable resources for making the text come alive.

Aerodynamics of Large Bridges

Aerodynamics of Large Bridges PDF Author: Allan Larsen
Publisher: Routledge
ISBN: 1351468057
Category : Technology & Engineering
Languages : en
Pages : 320

Book Description
As bridges spans get longer, lighter and more slender, aerodynamic loads become a matter of serious study. This volume of proceedings reflect the co-operation between civil and mechanical engineering and meteorology in this field.