NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 670

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 458

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Influence of Free-stream Disturbances on Boundary-layer Transition

Influence of Free-stream Disturbances on Boundary-layer Transition PDF Author: William D. Harvey
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

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Influence of Free-stream Disturbances on Boundary-layer Transition

Influence of Free-stream Disturbances on Boundary-layer Transition PDF Author: Bill Harvey
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 40

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A Collection of Technical Papers

A Collection of Technical Papers PDF Author:
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 1060

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Laminar-turbulent Transition

Laminar-turbulent Transition PDF Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
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ISBN:
Category : Aeronautics
Languages : en
Pages : 414

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In-flight Transition Measurement on a 100 Cone at Mach Numbers from 0.5 to 2.0

In-flight Transition Measurement on a 100 Cone at Mach Numbers from 0.5 to 2.0 PDF Author: David F. Fisher
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ISBN:
Category : Boundary layer
Languages : en
Pages : 148

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Artificially Induced Boundary-layer Transition on Blunt-slender Cones Using Distributed Roughness and Spherical-type Tripping Devices at Hypersonic Speeds

Artificially Induced Boundary-layer Transition on Blunt-slender Cones Using Distributed Roughness and Spherical-type Tripping Devices at Hypersonic Speeds PDF Author: Albert H. Boudreau
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 50

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Research directed toward establishing criteria for distributed roughness-type boundary-layer trips on blunt-slender cones has been conducted in the AEDC/VKF at Mach numbers from 8 to 13. Results indicate that distributed roughness trips are superior to spherical-type trips in that equally effective distributed roughness trips are one-fifth as high and produce substantially smaller flow-field disturbances. Criteria are defined for optimum utilization of distributed roughness trips.

Advisory Group for Aerospace Research and Development Index of Publications

Advisory Group for Aerospace Research and Development Index of Publications PDF Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 446

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