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 PDF Download

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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

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 PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20

Book Description


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

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 PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20

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

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 PDF Author: David S. Shaw
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 26

Book Description


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

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 PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 32

Book Description


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

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 PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Hypersonic wind tunnels
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

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 PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 72

Book Description


Low-Speed Wind Tunnel Testing

Low-Speed Wind Tunnel Testing PDF Author: Jewel B. Barlow
Publisher: 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.

China's Strategic Modernization Implications for the United States

China's Strategic Modernization Implications for the United States PDF Author: Mark A. Stokes
Publisher: DIANE Publishing
ISBN: 1428911979
Category : Air defenses
Languages : en
Pages : 230

Book Description
Conventional wisdom portrays the People's Republic of China (PRC) People's Liberation Army (PLA) as a backward continental force that will not pose a military challenge to its neighbors or to the United States well into the 21st century. PLA writings that demonstrate interest in exploiting the revolution in military affairs (RMA) are dismissed by a large segment of the PLA- watching community as wistful fantasies. The author offers an alternative perspective by outlining emerging PLA operational concepts and a range of research and development projects that appear to have been heavily influenced by U.S. and Russian writings on the RMA. Fulfillment of the PLA's vision for the 21st century could have significant repercussions for U.S. interests in the Asia-Pacific region.

Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics PDF Author: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 516

Book Description


Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63

Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 PDF Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 28

Book Description


The Evolution of the Cruise Missile

The Evolution of the Cruise Missile PDF Author: Kenneth P. Werrell
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 308

Book Description