Aerodynamic Coefficients for the Six-Inch TVC (TVC6) Missile
Aerodynamic Coefficients for the Six-Inch TVC (TVC6) Missile
- New search for: W. H. Clark
- New search for: W. H. Clark
This report is a final report documenting the predictions of the static aerodynamic coefficients (normal and side force and pitch and yaw moments) used in computer simulations of the Navy's 6-inch-diameter thrust vector controlled ASRAAM candidate. Although the predictions described are for a specific missile configuration, the techniques used are sufficiently general to be applicable to a variety of slender bodies of revolution that are expected to fly at high angles of attack. (Author)
Document information
Aerodynamic Coefficients for the Six-Inch TVC (TVC6) Missile
1978
59 pages
Report
No indication
English
Air & Space-Launched Missiles , Air to air missiles , Aerodynamic characteristics , Thrust vector control systems , Angle of attack , Computer programming , Pitch(Motion) , Aerodynamic forces , Short range(Distance) , Bodies of revolution , Static stability , Aerodynamic coefficients , TVC-6 missiles , Short Range Air to Air Missiles
Similar titles
Missile aerodynamic sensitivity analysis
| AIAA | 1978
Missile aerodynamic sensitivity analysis
| Tema Archive | 1978