Download or read book Transonic Investigation of the Effects of Nose Bluntness Fineness Ratio Cone Angle and Base Shape on the Static Aerodynamic Characteristics of Short Blunt Cones at Angles of Attack to 1800 written by Cuyler W. Brooks and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Investigation of the Effects of Nose Bluntness Fineness Ratio Cone Angle and Base Shape on the Static Aerodynamic Characteristics of Short Blunt Cones at Angles of Attack to 1800 written by Cuyler W. Brooks and published by . This book was released on 1963 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Investigation of the Effects of Nose Bluntness Fineness Ratio Cone Angle and Base Shape on the Static Aerodynamic Characteristics of Short Blunt Cones at Angles of Attack to 180 Degrees written by Cuyler W. Brooks (Jr.) and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Investigation of the Effects of Nose Bluntness Fineness Ratio Cone Angle and Base Shape on the Static Aerodynamic Characteristics of Short Blunt Cones at Angles of Attack to 180 O written by Cuyler W. Brooks (Jr.) and published by . This book was released on 1963 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Investigation of the Effects of Nose Bluntness Fineness Ratio Cone Angle and Base Shape on the Static Aerodynamic Characteristics of Short Blunt Cones at Angles of Attack to 180 written by Cuyler W. Brooks and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Nose Bluntness Fineness Ratio Cone Angle and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1 57 1 80 and 2 16 and Angles of Attack Up to 180 written by David S. Shaw and published by . This book was released on 1963 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1964 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of Short Blunt Cones with Various Nose and Base Cone Angles at Mach Numbers from 0 6 to 5 5 and Angles of Attack to 180 Degrees written by Stuart L. Treon and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Aerodynamic Characteristics of Blunted Cones at Mach Numbers of 3 5 4 2 and 6 0 written by J. Wayne Keyes and published by . This book was released on 1964 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Nose cone Angle on the Transonic Aerodynamic Characteristics of a Blunt Cone Cylinder Body Having a Cylindrical Flared Or Blunt finned Afterbody written by Stuart L. Treon and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Nose Bluntness Fineness Ratio Cone Angle and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1 57 1 80 and 2 16 and Angles of Attack Up to 180 Degrees written by David S. Shaw and published by . This book was released on 1963 with total page 77 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA TN D 1781 written by David S. Shaw and published by . This book was released on 1963 with total page 77 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book U S Government Research Reports written by and published by . This book was released on 1963 with total page 254 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Nose Bluntness Cone Angle and Mach Number Effects on the Stability Derivatives of Slender Cones written by James T. Clay and published by . This book was released on 1967 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical and experimental study to evaluate the influence of spherical nose bluntness, of cone angle, c. g. location and Mach number on the stability characteristics in pitch of blunt slender cones was conducted. A 10- degree half-angle cone with nose bluntness ratios from .025 to .30 was investigated. The observed effect of the nose bluntness on the stability derivatives was quite similar to earlier results with a 5.6 degree half-angle cone. Again, a severe breakdown of the damping derivatives was found for large bluntness ratios. An estimate of the pitch-induced angles of attack for large bluntness ratios was based on the physics of the blast wave type flow. It was found that these induced angles differ from those applicable for pointed cones or for small bluntness ratios where the flow has mainly conical character. The tangent cone method in connection with these different types of pitch-induced angles of attack qualitatively predicts the observed breakdown of the damping derivatives.
Download or read book A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp and Blunt nose Cones Having Flat and Modified Bases written by Sandia Corporation and published by . This book was released on 1965 with total page 596 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1963 with total page 644 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of Short Blunt Cones with Various Nose and Base Cone Angles at Mach Numbers from 0 6 to 5 5 and Angles of Attack to 180 written by Stuart L. Treon and published by . This book was released on 1962 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:
