Scientific and Technical Aerospace Reports

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

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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 Paper

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

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NASA Technical Memorandum

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

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Laminar-turbulent Transition

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

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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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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
Publisher:
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.

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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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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