Pressure Measurements On Sharp And Blunt 5 And 15 Half Angle Cones At Mach Number 3 86 And Angles Of Attack To 100

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Index To Nasa Technical Publications

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07

Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with categories.

Monthly Catalog Of United States Government Publications

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Author :
language : en
Publisher:
Release Date : 1961

Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Government publications categories.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1974

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aeronautics categories.

Ingenier A Aeronautica Y Astron Utica

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Author :
language : es
Publisher:
Release Date : 1962

Ingenier A Aeronautica Y Astron Utica written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Aeronautics categories.

Pressure Measurements On Sharp And Blunt 5 Degreee And 15 Degree Half Angle Cones At Mach Number 3 86 And Angles Of Attack To 100 Degrees

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Author : James L. Amick
language : en
Publisher:
Release Date : 1961

Pressure Measurements On Sharp And Blunt 5 Degreee And 15 Degree Half Angle Cones At Mach Number 3 86 And Angles Of Attack To 100 Degrees written by James L. Amick and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Fluid mechanics categories.

Bulletin Signal Tique

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Author :
language : fr
Publisher:
Release Date : 1961

Bulletin Signal Tique written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aeronautics categories.

Pressure Measurements On Sharp And Blunt 5 And 15 Half Angle Cones At Mach Number 3 86 And Angles Of Attack To 100

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Author : James L. Amick
language : en
Publisher:
Release Date : 1961

Pressure Measurements On Sharp And Blunt 5 And 15 Half Angle Cones At Mach Number 3 86 And Angles Of Attack To 100 written by James L. Amick and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.

Pressure Measurements On Sharp And Blunt 5 Degreee And 15 Degree Half Angle Cones At Mach Number 3 86 And Angles Of Attack To 100 Degrees

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Author : James L. Amick
language : en
Publisher:
Release Date : 1961

Pressure Measurements On Sharp And Blunt 5 Degreee And 15 Degree Half Angle Cones At Mach Number 3 86 And Angles Of Attack To 100 Degrees written by James L. Amick and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.

Laminar Heat Transfer And Pressure Measurements At A Mach Number Of 6 On A Sharp And Blunt 15 Half Angle Cones At Angles Of Attack Up To 90

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Author : Raul Jorge Conti
language : en
Publisher:
Release Date : 1961

Laminar Heat Transfer And Pressure Measurements At A Mach Number Of 6 On A Sharp And Blunt 15 Half Angle Cones At Angles Of Attack Up To 90 written by Raul Jorge Conti and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Heat categories.

Two circulation conical configurations having 15° half-angles were tested in laminar boundary layer at a Mach number of 6 and angles of attack up to 90°. One cone had a sharp nose and a fineness ratio of 1.87 and the other had a spherically blunted nose with a bluntness ratio of 0.1428 and a fineness ratio of 1.66. Pressure measurements and schlieren pictures of the flow showed that near-conical flow existed above 70° high pressure areas were present near the base and the bow shock wave was considerably curved.

Laminar Heat Transfer And Pressure Measurements At A Mach Number Of 6 On Sharp And Blunt 15 Degree Half Angle Cones At Angles Of Attack Up To 90 Degrees

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Author : RAUL J. CONTI
language : en
Publisher:
Release Date : 1961

Laminar Heat Transfer And Pressure Measurements At A Mach Number Of 6 On Sharp And Blunt 15 Degree Half Angle Cones At Angles Of Attack Up To 90 Degrees written by RAUL J. CONTI and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.

Heat-transfer and pressure distributions were measured on sharp and blunt 15 degree half-angle cones. The flow was near conical on the windward side of the models up to an angle of attack of about 60 degrees. At angles of attack above 70 degrees the flow departed noticeably from conical characteristics. Heat-transfer and pressure measurements were found to agree satisfactorily with theories of simple application. At large angles of attack the effects of nose bluntness are very small in the region beyond two nose radii from the point of tangency. (Author).