An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9

An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9 PDF Author: Michael C. Fischer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 76

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Book Description
Boundary layer transition on nose cones at hypersonic speeds.

An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9

An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9 PDF Author: Michael C. Fischer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 76

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Book Description
Boundary layer transition on nose cones at hypersonic speeds.

An Experimental Investigation of Boundary-layer Transition on a 10 Degree Half-angle Cone at Mach 6.9

An Experimental Investigation of Boundary-layer Transition on a 10 Degree Half-angle Cone at Mach 6.9 PDF Author: Michael C. Fischer
Publisher:
ISBN:
Category :
Languages : en
Pages : 63

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An Experimental Investigation of Boundary-layer Transition on a 10° Half-angle Cone at Mach 6.9

An Experimental Investigation of Boundary-layer Transition on a 10° Half-angle Cone at Mach 6.9 PDF Author: Michael C. Fischer
Publisher:
ISBN:
Category :
Languages : en
Pages : 63

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Experimental Investigation of Boundary-layer Transition on a Cooled 7.5 Degrees Total-angle Cone at Mach 10

Experimental Investigation of Boundary-layer Transition on a Cooled 7.5 Degrees Total-angle Cone at Mach 10 PDF Author: Philip E. Everhart
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 1004

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Experimental Investigation of Boundary-layer Transition on a Cooled 7.5° Total-angle Cone at Mach 10

Experimental Investigation of Boundary-layer Transition on a Cooled 7.5° Total-angle Cone at Mach 10 PDF Author: Philip E. Everhart
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 42

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An Experimental Investigation of Boundary Layer Transition on a Cone at Angle of Attack

An Experimental Investigation of Boundary Layer Transition on a Cone at Angle of Attack PDF Author: A. Martellucci
Publisher:
ISBN:
Category :
Languages : en
Pages : 212

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Book Description
As the first part of the Strategic Re-entry Technology (STREET G) task to determine the effect of asymmetric transition on static stability, an experimental investigation of the influence of angle of attack on boundary layer transition from location and shape has been conducted at AEDC Tunnel B at Mach 8. The model was a stainless steel 7.2 deg half-angle cone with three bluntness ratios. For each of the bluntness ratios, heat transfer data were obtained for four values of the free stream Reynolds number and for four angles of attack, that is, alpha = 0 deg, 1 deg, 2 deg, and 4 deg. Comparisons of the heat transfer at alpha = o deg were made with theory and good agreement resulted.

An Experimental Investigation on Unit Reynolds Number and Bluntness Effects on Boundary-layer Transition for a 10° Half-angle Cone at M[infinity]

An Experimental Investigation on Unit Reynolds Number and Bluntness Effects on Boundary-layer Transition for a 10° Half-angle Cone at M[infinity] PDF Author: Michael Carlton Fischer
Publisher:
ISBN:
Category :
Languages : en
Pages : 182

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A Study of Boundary Layer Transition on Outgassing Cones in Hypersonic Flow

A Study of Boundary Layer Transition on Outgassing Cones in Hypersonic Flow PDF Author:
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 92

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 816

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Book Description
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.