Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description
The Journal of the Royal Aeronautical Society
Author: Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster
Author: Albin O. PearsonPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
Journal of the Royal Aeronautical Society
Author: Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.14 of the Static Aerodynamic Characteristics of a Model of a Project Mercury Capsule
Author: Albin O. PearsonPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 32
Book Description
Wind-tunnel Investigation of Static Aerodynamic Characteristics of a 1/9-scale Model of a Possible Reentry Capsule at Mach Numbers from 2.29 to 4.65
Author: David S. ShawPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 26
Book Description
Wind-tunnel Investigation at Mach Numbers from 0.40 to 1.20 of the Static Aerodynamic and Control Characteristics of a Model of a Nonlifting Reeintry Capsule in Combination with a Rocket Booster
Author: Albin O. PearsonPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 72
Book Description
Low-Speed Wind Tunnel Testing
Author: Jewel B. BarlowPublisher: John Wiley & Sons
ISBN: 0471557749
Category : Technology & Engineering
Languages : en
Pages : 738
Book Description
A brand-new edition of the classic guide on low-speed wind tunnel testing While great advances in theoretical and computational methods have been made in recent years, low-speed wind tunnel testing remains essential for obtaining the full range of data needed to guide detailed design decisions for many practical engineering problems. This long-awaited Third Edition of William H. Rae, Jr.'s landmark reference brings together essential information on all aspects of low-speed wind tunnel design, analysis, testing, and instrumentation in one easy-to-use resource. Written by authors who are among the most respected wind tunnel engineers in the world, this edition has been updated to address current topics and applications, and includes coverage of digital electronics, new instrumentation, video and photographic methods, pressure-sensitive paint, and liquid crystal-based measurement methods. The book is organized for quick access to topics of interest, and examines basic test techniques and objectives of modeling and testing aircraft designs in low-speed wind tunnels, as well as applications to fluid motion analysis, automobiles, marine vessels, buildings, bridges, and other structures subject to wind loading. Supplemented with real-world examples throughout, Low-Speed Wind Tunnel Testing, Third Edition is an indispensable resource for aerospace engineering students and professionals, engineers and researchers in the automotive industries, wind tunnel designers, architects, and others who need to get the most from low-speed wind tunnel technology and experiments in their work.
Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations
Author: Albin O. PearsonPublisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 26
Book Description
Hypersonic and High Temperature Gas Dynamics
Author: John David AndersonPublisher: AIAA
ISBN: 9781563474590
Category : Science
Languages : en
Pages : 710
Book Description
This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Handbook of Supersonic Aerodynamics
Author: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, MdPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 516
Book Description