Artificially Induced Boundary Layer Transition On Blunt Slender Cones Using Distributed Roughness And Spherical Type Tripping Devices At Hypersonic Speeds


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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

Author: Albert H. Boudreau

language: en

Publisher:

Release Date: 1978


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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.

Scientific and Technical Aerospace Reports


Scientific and Technical Aerospace Reports

Author:

language: en

Publisher:

Release Date: 1978


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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.