Aerodynamic Characteristics at a Mach Number of 6.77 of a 9 ̊cone Configuration, with and Without Spherical Afterbodies, at Angles of Attack Up to 180 ̊with Various Degrees of Nose Blunting
| Title | Aerodynamic Characteristics at a Mach Number of 6.77 of a 9 ̊cone Configuration, with and Without Spherical Afterbodies, at Angles of Attack Up to 180 ̊with Various Degrees of Nose Blunting PDF eBook |
| Author | Luther Neal (Jr.) |
| Publisher | |
| Pages | 32 |
| Release | 1963 |
| Genre | Aerodynamic load |
| ISBN |
Download Aerodynamic Characteristics at a Mach Number of 6.77 of a 9 ̊cone Configuration, with and Without Spherical Afterbodies, at Angles of Attack Up to 180 ̊with Various Degrees of Nose Blunting Book in PDF, Epub and Kindle
Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium
| Title | Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium PDF eBook |
| Author | Melvin J. Fohrman |
| Publisher | |
| Pages | 48 |
| Release | 1963 |
| Genre | Aerodynamics |
| ISBN |
Download Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium Book in PDF, Epub and Kindle
Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300
| Title | Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 PDF eBook |
| Author | Jim A. Penland |
| Publisher | |
| Pages | 50 |
| Release | 1961 |
| Genre | Mach number |
| ISBN |
Download Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 Book in PDF, Epub and Kindle
Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85
| Title | Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 PDF eBook |
| Author | Lucille C. Coltrane |
| Publisher | |
| Pages | 32 |
| Release | 1962 |
| Genre | Aircraft |
| ISBN |
Download Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 Book in PDF, Epub and Kindle
A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp-and Blunt-nose Cones Having Flat and Modified Bases
| Title | A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp-and Blunt-nose Cones Having Flat and Modified Bases PDF eBook |
| Author | Sandia Corporation |
| Publisher | |
| Pages | 596 |
| Release | 1965 |
| Genre | Aerodynamics |
| ISBN |
Download A Compilation of Longitudinal Aerodynamic Characteristics Including Pressure Information for Sharp-and Blunt-nose Cones Having Flat and Modified Bases Book in PDF, Epub and Kindle
Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180°
| Title | Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° PDF eBook |
| Author | Leroy Devan |
| Publisher | |
| Pages | 192 |
| Release | 1980 |
| Genre | Angle of attack (Aerodynamics). |
| ISBN |
Download Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° Book in PDF, Epub and Kindle
Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares
| Title | Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares PDF eBook |
| Author | A. B. Carraway |
| Publisher | |
| Pages | 124 |
| Release | 1960 |
| Genre | |
| ISBN |
Download Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares Book in PDF, Epub and Kindle