Viscous and Interacting Flow Field Effects

Viscous and Interacting Flow Field Effects PDF Author:
Publisher:
ISBN:
Category : Turbulent boundary layer
Languages : en
Pages : 316

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25th AIAA Fluid Dynamics Conference

25th AIAA Fluid Dynamics Conference PDF Author:
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 586

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 104

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32nd Aerospace Sciences Meeting & Exhibit: 94-0001 - 94-0029

32nd Aerospace Sciences Meeting & Exhibit: 94-0001 - 94-0029 PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 460

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Base Bleed

Base Bleed PDF Author: Kenneth K. Kuo
Publisher: Taylor & Francis
ISBN: 9780891169376
Category : Science
Languages : en
Pages : 336

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Book Description
Includes papers presented at a symposium, which represent the state-of-the-art in the development of base bleed projectiles and related research, and are from recognized experts in the field. The papers have undergone a thorough review process.

Experimental and Theoretical Studies of Axisymmetric Free Jets

Experimental and Theoretical Studies of Axisymmetric Free Jets PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 300

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Book Description
Some experimental and theoretical studies have been made of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams with a view toward problems associated with propulsive jets and the investigation of these problems. For jets exhausting into still air, consideration is given to the effects of jet Mach number, nozzle divergence angle, and jet static-pressure ratio upon jet structure, jet wavelength, and the shape and curvature of the jet boundary. Studies of the effects of the ratio of specific heats of the jets are included as are observations pertaining to jet noise and jet simulation. For jets exhausting into supersonic streams, an attempt has been made to present primarily theoretical curves of the type that may be useful in evaluating certain jet interference effects and in formulating experimental studies. The primary variables considered are jet Mach number, free-stream Mach number, jet static-pressure ratio, ratio of specific heats of the jet, nozzle exit angle, and boattail angle. The simulation problem and the case of a hypothetical hypersonic vehicle are examined. A few experimental observations are included.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 700

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

AIAA Journal

AIAA Journal PDF Author: American Institute of Aeronautics and Astronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1184

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R & D Abstracts

R & D Abstracts PDF Author: Technology Reports Centre (Great Britain)
Publisher:
ISBN:
Category :
Languages : en
Pages : 682

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26th AIAA Fluid Dynamics Conference

26th AIAA Fluid Dynamics Conference PDF Author:
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 478

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