Boundary-layer Velocity Profiles Downstream of Three-dimensional Transition Trips on a Flat Plate at Mach 3 and 4

Boundary-layer Velocity Profiles Downstream of Three-dimensional Transition Trips on a Flat Plate at Mach 3 and 4 PDF Author: John B. Peterson
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 100

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Boundary layer velocity profiles downstream of three dimensional transition trips on flat plates at Mach 3 and 4.

Boundary-layer Velocity Profiles Downstream of Three-dimensional Transition Trips on a Flat Plate at Mach 3 and 4

Boundary-layer Velocity Profiles Downstream of Three-dimensional Transition Trips on a Flat Plate at Mach 3 and 4 PDF Author: John B. Peterson
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 100

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Book Description
Boundary layer velocity profiles downstream of three dimensional transition trips on flat plates at Mach 3 and 4.

Boundary-layer Velocity Profiles Downstream of Three-dimensional Transition Trips on a Flat Plate at Mach 3 and 4

Boundary-layer Velocity Profiles Downstream of Three-dimensional Transition Trips on a Flat Plate at Mach 3 and 4 PDF Author: John B. Peterson
Publisher:
ISBN:
Category :
Languages : en
Pages : 87

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 736

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Scientific and Technical Aerospace Reports

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

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Boundary-layer Transition Study of Several Pointed Bodies of Revolution at Supersonic Speeds

Boundary-layer Transition Study of Several Pointed Bodies of Revolution at Supersonic Speeds PDF Author: William A. Cassels
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 76

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Boundary-layer transition by the sublimation and impact-pressure techniques and force tests have been performed on three Haack-Adams bodies of revolution of fineness ratios 7, 10, and 13 at zero angle of attack for free-stream Mach numbers of 2.00, 2.75, and 4.63 and a range of Reynolds numbers based on model length of 6 to 15 X 10(to the 6 power) with and without a roughness strip. The grit method of inducing turbulence was found to provide for a nearly complete turbulent flow over the models at the lower Mach numbers and higher Reynolds numbers considered in this study while the amount of trip drag was less than 8 percent of the model drag with transition fixed. A method of interpreting sublimation data was discussed and used and the results compared well with the impact-pressure results.

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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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340

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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 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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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 496

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