Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00
DOWNLOAD
Download Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00 PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00 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
The Aeronautical Journal
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1969
The Aeronautical Journal written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aeronautics categories.
Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Degree Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00
DOWNLOAD
Author : Robert J. McGhee
language : en
Publisher:
Release Date : 1969
Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Degree Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00 written by Robert J. McGhee and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with categories.
Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00
DOWNLOAD
Author : Robert J. McGhee
language : en
Publisher:
Release Date : 1969
Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00 written by Robert J. McGhee and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Blunt bodies categories.
Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00
DOWNLOAD
Author : Robert J. MacGhee
language : en
Publisher:
Release Date : 1969
Aerodynamic Investigation Of Sharp Cone Cylinder Spikes On 120 Blunted Cones At Mach Numbers Of 3 00 4 50 And 6 00 written by Robert J. MacGhee and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 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.
Measured And Predicted Shock Shapes And Aerodynamic Coefficients For Blunted Cones At Incidence In Helium At Mach 20 3
DOWNLOAD
Author : Robert L. Calloway
language : en
Publisher:
Release Date : 1979
Measured And Predicted Shock Shapes And Aerodynamic Coefficients For Blunted Cones At Incidence In Helium At Mach 20 3 written by Robert L. Calloway and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Aerodynamics, Hypersonic categories.
Experimental values of shock shapes (alpha = 0 degrees and 10 degrees) and static aerodynamic coefficients (alpha = -4 degrees to 12 degrees) for sharp and spherically blunted cones having cone half-angles of 30, 45, 60, and 70 degrees and nose bluntness ratios of 0, 0.25, and 0.50 are presented. Shock shapes were also measured at 0 degree angle of attack by using a flat-faced cylinder (90 degree cone) and a hemispherically blunted cylinder (sphere). All tests were conducted in helium (gamma = 5/3) at a free-stream Mach number of 20.3 and a unit free-stream Reynolds number of 22,400,000 per meter. Comparisons between measured values and predicted values were made by using several numerical and simple engineering methods.
Flow Field Investigation For Large Angle Cones With Short Spikes At A Mach Number Of 9 6
DOWNLOAD
Author : W. Frank Staylor
language : en
Publisher:
Release Date : 1970
Flow Field Investigation For Large Angle Cones With Short Spikes At A Mach Number Of 9 6 written by W. Frank Staylor and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Blunt bodies categories.
Pressure Distributions And Aerodynamic Characteristics Of 90 And 150 Blunted Cones In Nitrogen And Helium At Mach 20
DOWNLOAD
Author : Theodore R. Creel
language : en
Publisher:
Release Date : 1968
Pressure Distributions And Aerodynamic Characteristics Of 90 And 150 Blunted Cones In Nitrogen And Helium At Mach 20 written by Theodore R. Creel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Aerodynamic load categories.
Force And Pressure Tests On Cones With Simulated Ablated Noses At Mach Numbers 8 And 16
DOWNLOAD
Author : J. S. Hahn
language : en
Publisher:
Release Date : 1972
Force And Pressure Tests On Cones With Simulated Ablated Noses At Mach Numbers 8 And 16 written by J. S. Hahn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Ablation (Aerothermodynamics) categories.
Aerodynamic Characteristics Of Spherically Blunted Cones At Mach Numbers From 0 5 To 5 0
DOWNLOAD
Author : Robert V. Owens
language : en
Publisher:
Release Date : 1965
Aerodynamic Characteristics Of Spherically Blunted Cones At Mach Numbers From 0 5 To 5 0 written by Robert V. Owens and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamics categories.