Author: Witold Nowacki
Publisher:
ISBN:
Category : Structural dynamics
Languages : en
Pages : 402
Book Description
Dynamics of Elastic Systems
Author: Witold Nowacki
Publisher:
ISBN:
Category : Structural dynamics
Languages : en
Pages : 402
Book Description
Publisher:
ISBN:
Category : Structural dynamics
Languages : en
Pages : 402
Book Description
Axial Flow Turbines
Author: J. H. Horlock
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 275
Book Description
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 275
Book Description
Thermodynamics I
Author: John R. Dixon
Publisher: Prentice Hall
ISBN:
Category : Science
Languages : en
Pages : 488
Book Description
Publisher: Prentice Hall
ISBN:
Category : Science
Languages : en
Pages : 488
Book Description
Steam Turbine Theory and Practice - a Textbook for Engineering Students
Author: F. H. Titmuss
Publisher: Aristophanes Press
ISBN: 9781447439134
Category : Technology & Engineering
Languages : en
Pages : 536
Book Description
Many of the earliest books, particularly those dating back to the 1900s and before, are now extremely scarce and increasingly expensive. We are republishing these classic works in affordable, high quality, modern editions, using the original text and artwork.
Publisher: Aristophanes Press
ISBN: 9781447439134
Category : Technology & Engineering
Languages : en
Pages : 536
Book Description
Many of the earliest books, particularly those dating back to the 1900s and before, are now extremely scarce and increasingly expensive. We are republishing these classic works in affordable, high quality, modern editions, using the original text and artwork.
Cascade Aerodynamics
Author: J. P. Gostelow
Publisher: Pergamon
ISBN:
Category : Science
Languages : en
Pages : 296
Book Description
Good,No Highlights,No Markup,all pages are intact, Slight Shelfwear,may have the corners slightly dented, may have slight color changes/slightly damaged spine.
Publisher: Pergamon
ISBN:
Category : Science
Languages : en
Pages : 296
Book Description
Good,No Highlights,No Markup,all pages are intact, Slight Shelfwear,may have the corners slightly dented, may have slight color changes/slightly damaged spine.
NASA SP.
Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations
Author: George L. Pratt
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 110
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 110
Book Description
Fundamentals of Turbomachinery
Author: William W. Peng
Publisher: John Wiley & Sons
ISBN: 0470124229
Category : Technology & Engineering
Languages : en
Pages : 386
Book Description
A comprehensive introduction to turbomachines and their applications With up-to-date coverage of all types of turbomachinery for students and practitioners, Fundamentals of Turbomachinery covers machines from gas, steam, wind, and hydraulic turbines to simple pumps, fans, blowers, and compressors used throughout industry. After reviewing the history of turbomachinery and the fluid mechanical principles involved in their design and operation, the book focuses on the application and selection of machines for various uses, teaching basic theory as well as how to select the right machine for a specific use. With a practical emphasis on engineering applications of turbomachines, this book discusses the full range of both turbines and pumping devices. For each type, the author explains: * Basic principles * Preliminary design procedure * Ideal performance characteristics * Actual performance curves published by the manufacturers * Application and appropriate selection of the machine Throughout, worked sample problems illustrate the principles discussed and end-of-chapter problems, employing both SI and the English system of units, provide practice to help solidify the reader's grasp of the material.
Publisher: John Wiley & Sons
ISBN: 0470124229
Category : Technology & Engineering
Languages : en
Pages : 386
Book Description
A comprehensive introduction to turbomachines and their applications With up-to-date coverage of all types of turbomachinery for students and practitioners, Fundamentals of Turbomachinery covers machines from gas, steam, wind, and hydraulic turbines to simple pumps, fans, blowers, and compressors used throughout industry. After reviewing the history of turbomachinery and the fluid mechanical principles involved in their design and operation, the book focuses on the application and selection of machines for various uses, teaching basic theory as well as how to select the right machine for a specific use. With a practical emphasis on engineering applications of turbomachines, this book discusses the full range of both turbines and pumping devices. For each type, the author explains: * Basic principles * Preliminary design procedure * Ideal performance characteristics * Actual performance curves published by the manufacturers * Application and appropriate selection of the machine Throughout, worked sample problems illustrate the principles discussed and end-of-chapter problems, employing both SI and the English system of units, provide practice to help solidify the reader's grasp of the material.
Unsteady Transonic Aerodynamics
Author: David Nixon
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 410
Book Description
This volume complements Transonic aerodynamics (v.81 in the series) which is concerned with steady flow. This is the only book to address the subject of unsteady transonic aerodynamics, a field much different from steady aerodynamics. The most pronounced difference is the complex shock wave motions
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 410
Book Description
This volume complements Transonic aerodynamics (v.81 in the series) which is concerned with steady flow. This is the only book to address the subject of unsteady transonic aerodynamics, a field much different from steady aerodynamics. The most pronounced difference is the complex shock wave motions
Effects of Wing-tip Droop on the Longitudinal Characteristics of Two Highly Swept Wing-body Combinations at Mach Numbers from 0.6 to 1.4
Author: Earl D. Knechtel
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description
An investigation was conducted to determine the effects of wing-tip droop on the longitudinal stability characteristics of a 53 and a 63 degree sweptback wing-body combination. Both models were tested with flat and abruptly drooped wing tips. The 63 degree wing was also tested with a curved drooped tip. In addition, the combined effects of wing fences and extended leading-edge flaps were investigated. The results showed that abrupt droop of the outer 40 percent of the basic 53 degree wing improved the stability characteristics of the model. For the 63 degree swept wing, curved droop caused slight beneficial effects on the stability, whereas abrupt droop caused adverse effects. In general, the most favorable stability characteristics were obtained for either flat or abruptly drooped wings with fences and extended leading-edge flaps.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description
An investigation was conducted to determine the effects of wing-tip droop on the longitudinal stability characteristics of a 53 and a 63 degree sweptback wing-body combination. Both models were tested with flat and abruptly drooped wing tips. The 63 degree wing was also tested with a curved drooped tip. In addition, the combined effects of wing fences and extended leading-edge flaps were investigated. The results showed that abrupt droop of the outer 40 percent of the basic 53 degree wing improved the stability characteristics of the model. For the 63 degree swept wing, curved droop caused slight beneficial effects on the stability, whereas abrupt droop caused adverse effects. In general, the most favorable stability characteristics were obtained for either flat or abruptly drooped wings with fences and extended leading-edge flaps.