Author: H. Merbt
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Aerodynamic Forces on Oscillating Low Aspect Ratio Wings in Compressible Flow
The Unsteady Aerodynamic Forces on Deforming, Low Aspect Ratio Wings and Slender Wing-body Combinations Oscillating Harmonically in a Compressible Flow, by R.D. Milne
Author: Ronald D. Milne
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 42
Book Description
THE UNSTEASY AERODYNAMIC FORCES ON DEFORMING, LOW ASPECT RATIO WINGS AND SLENDER WING-BODY COMBINATIONS OSCILLATING HARMONICALLY IN A COMPRESSIBLE FLOW.
The Aerodynamic Forces on Low-aspect-ratio Wings Oscillating in an Incompressible Flow
Measurement of Aerodynamic Forces on an Oscillating Airfoil
Author: Richard I. Windsor
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 252
Book Description
A literature survey was conducted to determine the state of the art of measuring and predicting aerodynamic characteristics of oscillating air-foils. Aerodynamic forces on a two-dimensional NACA 0012 airfoil oscillating sinusoidally in pitch were measured by two techniques. The forces were obtained from pressure measurements and by means of strain gage balances. Pressure measurements were made on the airfoil oscillating in pitch about the quarter-chord point at various mean angles of attack. Strain gage balance readings were obtained for models with pitch axis located at 25, 37, and 50 percent chord points oscillating about various mean angles. Direct force measurements were employed in an effort to obtain drag data. Instantaneous pressure distributions are presneted for representative oscillating conditions. (Author).
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 252
Book Description
A literature survey was conducted to determine the state of the art of measuring and predicting aerodynamic characteristics of oscillating air-foils. Aerodynamic forces on a two-dimensional NACA 0012 airfoil oscillating sinusoidally in pitch were measured by two techniques. The forces were obtained from pressure measurements and by means of strain gage balances. Pressure measurements were made on the airfoil oscillating in pitch about the quarter-chord point at various mean angles of attack. Strain gage balance readings were obtained for models with pitch axis located at 25, 37, and 50 percent chord points oscillating about various mean angles. Direct force measurements were employed in an effort to obtain drag data. Instantaneous pressure distributions are presneted for representative oscillating conditions. (Author).
Principles of Aeroelasticity
Author: Raymond L. Bisplinghoff
Publisher: Courier Corporation
ISBN: 0486783162
Category : Technology & Engineering
Languages : en
Pages : 545
Book Description
Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.
Publisher: Courier Corporation
ISBN: 0486783162
Category : Technology & Engineering
Languages : en
Pages : 545
Book Description
Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.
The Aerodynamic Pressures on a Harmonically Oscillating Rectangular Wing
Author: John Lewis Troutman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 154
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 154
Book Description
Calculation of Lifting Forces on Oscillating Wings
Author: Valter J. E. Stark
Publisher:
ISBN:
Category : Airplane wings
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Airplane wings
Languages : en
Pages : 32
Book Description
Wing Theory
Author: A. Robinson
Publisher: Cambridge University Press
ISBN: 1107622654
Category : Technology & Engineering
Languages : en
Pages : 583
Book Description
First published in 1956 as part of the Cambridge Aeronautical Series, this book addresses the vital science of wing theory. Robinson and Laurmann record the historic developments in wing theory, including the work of Joukowski and Bernoulli, and discuss developments in supersonic flow and unsteady aerofoil theory. This book will be of value to anyone with an interest in the history of the science of flight.
Publisher: Cambridge University Press
ISBN: 1107622654
Category : Technology & Engineering
Languages : en
Pages : 583
Book Description
First published in 1956 as part of the Cambridge Aeronautical Series, this book addresses the vital science of wing theory. Robinson and Laurmann record the historic developments in wing theory, including the work of Joukowski and Bernoulli, and discuss developments in supersonic flow and unsteady aerofoil theory. This book will be of value to anyone with an interest in the history of the science of flight.
An Introduction to the Theory of Aeroelasticity
Author: Y C Fung
Publisher: Courier Dover Publications
ISBN: 0486469360
Category : Technology & Engineering
Languages : en
Pages : 516
Book Description
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
Publisher: Courier Dover Publications
ISBN: 0486469360
Category : Technology & Engineering
Languages : en
Pages : 516
Book Description
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.