Static Pressure on Sharp and Blunt Cones in Conical and Parallel Low-density Flow

Static Pressure on Sharp and Blunt Cones in Conical and Parallel Low-density Flow PDF Author: Max Kinslow
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 78

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Book Description
The static pressure distribution on sharp and blunt 10-deg half-angle cones was measured under rarefied conditions in both a uniform and a source flow field. Angle of attack of the cones was varied up to 10 deg. Pressure distributions are presented for cold-wall conditions at 18.0 = or

Static Pressure on Sharp and Blunt Cones in Conical and Parallel Low-density Flow

Static Pressure on Sharp and Blunt Cones in Conical and Parallel Low-density Flow PDF Author: Max Kinslow
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 78

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Book Description
The static pressure distribution on sharp and blunt 10-deg half-angle cones was measured under rarefied conditions in both a uniform and a source flow field. Angle of attack of the cones was varied up to 10 deg. Pressure distributions are presented for cold-wall conditions at 18.0 = or

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1074

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Government Reports Announcements

Government Reports Announcements PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages :

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Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow

Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow PDF Author: David E. Boylan
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 68

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Book Description
The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9 and +10 deg in a low-density, hypersonic wind tunnel. Circumferential and longitudinal distributions are presented for cold wall conditions for a range at Mach and Reynolds numbers. The effect of source-like flows was studied by utilizing both conical and contoured expansion nozzles with the same free-stream similarity parameters and model wall temperatures. Comparisons are made with previously published experimental and theoretical results. (Author).

Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 290

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Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

Government Reports Annual Index

Government Reports Annual Index PDF Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882

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Outer Planet Entry Heating and Thermal Protection

Outer Planet Entry Heating and Thermal Protection PDF Author: Raymond Viskanta
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 432

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Government Reports Index

Government Reports Index PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1076

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Numerical Methods in Laminar and Turbulent Flow

Numerical Methods in Laminar and Turbulent Flow PDF Author: Cedric Taylor
Publisher:
ISBN:
Category : Mathematics
Languages : en
Pages : 1032

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450

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