Effects of Several Nose and Vertical-fin Modifications on the Low-angle-of-attack Static Stability of a Winged Reentry Vehicle at Mach Numbers of 9.6 in Air and 17.8 in Helium
| Title | Effects of Several Nose and Vertical-fin Modifications on the Low-angle-of-attack Static Stability of a Winged Reentry Vehicle at Mach Numbers of 9.6 in Air and 17.8 in Helium PDF eBook |
| Author | |
| Publisher | |
| Pages | 52 |
| Release | 1961 |
| Genre | |
| ISBN |
Download Effects of Several Nose and Vertical-fin Modifications on the Low-angle-of-attack Static Stability of a Winged Reentry Vehicle at Mach Numbers of 9.6 in Air and 17.8 in Helium Book in PDF, Epub and Kindle
Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1.50, 2.96, and 4.63
| Title | Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1.50, 2.96, and 4.63 PDF eBook |
| Author | |
| Publisher | |
| Pages | 78 |
| Release | 1962 |
| Genre | |
| ISBN |
Download Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1.50, 2.96, and 4.63 Book in PDF, Epub and Kindle
Summary of Aerodynamic Characteristics of a Winged Reentry Vehicle at Mach Numbers from 0.06 to 9.6 with Detailed Results at a Mach Number of 9.6
| Title | Summary of Aerodynamic Characteristics of a Winged Reentry Vehicle at Mach Numbers from 0.06 to 9.6 with Detailed Results at a Mach Number of 9.6 PDF eBook |
| Author | |
| Publisher | |
| Pages | 68 |
| Release | 1963 |
| Genre | |
| ISBN |
Download Summary of Aerodynamic Characteristics of a Winged Reentry Vehicle at Mach Numbers from 0.06 to 9.6 with Detailed Results at a Mach Number of 9.6 Book in PDF, Epub and Kindle
Some Effects of Fin Plan Form on the Static Stability of Fin-body Combinations at Mach Number 4.06
| Title | Some Effects of Fin Plan Form on the Static Stability of Fin-body Combinations at Mach Number 4.06 PDF eBook |
| Author | Edward F. Ulmann |
| Publisher | |
| Pages | 28 |
| Release | 1952 |
| Genre | Aerodynamics, Supersonic |
| ISBN |
Download Some Effects of Fin Plan Form on the Static Stability of Fin-body Combinations at Mach Number 4.06 Book in PDF, Epub and Kindle
Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82
| Title | Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 PDF eBook |
| Author | Ross B. Robinson |
| Publisher | |
| Pages | 42 |
| Release | 1959 |
| Genre | Mach number |
| ISBN |
Download Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 Book in PDF, Epub and Kindle
Studies of Stability and Control of Winged Reentry Configurations
| Title | Studies of Stability and Control of Winged Reentry Configurations PDF eBook |
| Author | |
| Publisher | |
| Pages | 20 |
| Release | 1960 |
| Genre | |
| ISBN |
Download Studies of Stability and Control of Winged Reentry Configurations Book in PDF, Epub and Kindle
An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence
| Title | An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence PDF eBook |
| Author | John A. Axelson |
| Publisher | |
| Pages | 20 |
| Release | 1948 |
| Genre | Aeronautics |
| ISBN |
Download An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence Book in PDF, Epub and Kindle
An analysis is presented of the influence of wing aspect ratio and tail location on the effects of compressibility upon static longitudinal stability. The investigation showed that the use of reduced wing aspect ratios or short tail lengths leads to serious reductions in high-speed stability and the possibility of high-speed instability.