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
DOWNLOAD
Download 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 PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get 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 book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Technical Abstract Bulletin
DOWNLOAD
Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1962
Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Technology categories.
U S Government Research Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1962
U S Government Research 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 1962 with Science categories.
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
DOWNLOAD
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).
Scientific And Technical Aerospace Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1966
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 1966 with Aeronautics categories.
Bibliography Of Scientific And Industrial Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1962
Bibliography Of Scientific And Industrial 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 1962 with Science categories.
Government Wide Index To Federal Research Development Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1966
Government Wide Index To Federal Research Development 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 1966 with Government publications 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
DOWNLOAD
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 Measurement At A Mach Number Of 6 On Sharp And Blunt 15 Half Angle Cones At Angles Of Attack Up To 90
DOWNLOAD
Author : Raul J. Conti
language : en
Publisher:
Release Date : 1961
Laminar Heat Transfer And Pressure Measurement At A Mach Number Of 6 On Sharp And Blunt 15 Half Angle Cones At Angles Of Attack Up To 90 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.
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
DOWNLOAD
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.
Measurements Of Pressure And Local Heat Transfer On A 20 Degree Cone At Angles Of Attack Up To 20 Degrees For A Mach Number Of 4 95
DOWNLOAD
Author : Jerome D. Julius
language : en
Publisher:
Release Date : 1959
Measurements Of Pressure And Local Heat Transfer On A 20 Degree Cone At Angles Of Attack Up To 20 Degrees For A Mach Number Of 4 95 written by Jerome D. Julius and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.