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NASA Technical Note

NASA Technical Note PDF Author:
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ISBN:
Category :
Languages : en
Pages : 630

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Influence of Suction on Shock Wave-turbulent Boundary Layer Interactions for Two-dimensional and Axially Symmetric Flows

Influence of Suction on Shock Wave-turbulent Boundary Layer Interactions for Two-dimensional and Axially Symmetric Flows PDF Author: William R. Seebaugh
Publisher:
ISBN:
Category : Head waves
Languages : en
Pages : 148

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Influence of Suction on Shock Wave-turbulent Boundary Layer Interactions for Two- Dimensional and Axially Symmetric Flows, 16 September 1967 - 30 June 1969

Influence of Suction on Shock Wave-turbulent Boundary Layer Interactions for Two- Dimensional and Axially Symmetric Flows, 16 September 1967 - 30 June 1969 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 148

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 630

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836

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Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1504

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1730

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
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ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 300

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Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference

Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference PDF Author:
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ISBN:
Category : Airplanes
Languages : en
Pages : 442

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Investigation of Flow Fields Within Large-scale Hypersonic Inlet Models

Investigation of Flow Fields Within Large-scale Hypersonic Inlet Models PDF Author: A. Vernon Gnos
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 180

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Analytical and experimental investigations were conducted to determine the internal flow characteristics in model passages representative of hypersonic inlets for use at Mach numbers to about 12. The passages were large enough to permit measurements to be made in both the core flow and boundary layers. The analytical techniques for designing the internal contours and predicting the internal flow-field development accounted for coupling between the boundary layers and inviscid flow fields by means of a displacement-thickness correction. Three large-scale inlet models, each having a different internal compression ratio, were designed to provide high internal performance with an approximately uniform static-pressure distribution at the throat station. The models were tested in the Ames 3.5-Foot Hypersonic Wind Tunnel at a nominal free-stream Mach number of 7.4 and a unit free-stream Reynolds number of 8.86 X one million per meter.

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1464

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