Body Alone Aerodynamics of Guided and Unguided Projectiles at Subsonic, Transonic and Supersonic Mach Numbers
Title | Body Alone Aerodynamics of Guided and Unguided Projectiles at Subsonic, Transonic and Supersonic Mach Numbers PDF eBook |
Author | |
Publisher | |
Pages | 121 |
Release | 1972 |
Genre | |
ISBN |
Several theoretical and empirical methods are combined into a single computer program to predict lift, drag, and center of pressure on bodies of revolution at subsonic, transonic, and supersonic Mach numbers. The body geometries can be quite general in that pointed, spherically blunt, or truncated noses are allowed as well as discontinuities in nose shape. Particular emphasis is placed on methods which yield accuracies of ninety percent or better for most configurations but yet are computationally fast. Theoretical and experimental results are presented for several projectiles and a computer program listing is included as an appendix.
Body Alone Aerodynamics of Guided and Unguide Projectiles at Subsonic, Transonic and Supersonic Mach Numbers
Title | Body Alone Aerodynamics of Guided and Unguide Projectiles at Subsonic, Transonic and Supersonic Mach Numbers PDF eBook |
Author | Frankie Gale Moore |
Publisher | |
Pages | 146 |
Release | 1972 |
Genre | Aerodynamics |
ISBN |
Several theoretical and empirical methods are comgined into a single computer program to predict lift, drag, and center of pressure on bodies of revolution at subsonic, transonic, and supersonic Mach numbers. The body geometries can be quite general in that pointed, spherically blunt, or truncated noses are allowed as well as discontinuities in nose shape. Particular emphasis is placed on methods which yield accuracies of ninety percent or better for most configurations but yet are computationally fast. theoretical and experimental results are presented for several projectiles and a computer program listing is included an an appendix.
Aerodynamics of Guided and Unguided Weapons
Title | Aerodynamics of Guided and Unguided Weapons PDF eBook |
Author | Frankie Gale Moore |
Publisher | |
Pages | 218 |
Release | 1973 |
Genre | Guided missiles |
ISBN |
Several theoretical and empirical procedures are combined into a single computer program to predict lift, drag, and center of pressure on quite general wing-body geometries. The method is applicable for Mach number zero to three and angle-of-attack zero to about fifteen degrees. Computed results for several configurations compare well with experimental and other analytical results. It costs about five dollars per Mach number to compute the static aerodynamics of a typical wing-body shape on the CDC 6700 computer.
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 |
Aerodynamic Design Manual for Tactical Weapons
Title | Aerodynamic Design Manual for Tactical Weapons PDF eBook |
Author | Lawrence Mason |
Publisher | |
Pages | 182 |
Release | 1981 |
Genre | Aerodynamics |
ISBN |
Aerodynamics of Tactical Weapons to Mach Number 3 and Angle of Attack 15
Title | Aerodynamics of Tactical Weapons to Mach Number 3 and Angle of Attack 15 PDF eBook |
Author | Roy C. Swanson (Jr.) |
Publisher | |
Pages | 192 |
Release | 1977 |
Genre | Aerodynamics |
ISBN |
State-of-the-art Engineering Aeroprediction Methods with Emphasis on New Semiempirical Techniques for Predicting Nonlinear Aerodynamics on Complete Missile Configurations
Title | State-of-the-art Engineering Aeroprediction Methods with Emphasis on New Semiempirical Techniques for Predicting Nonlinear Aerodynamics on Complete Missile Configurations PDF eBook |
Author | Frankie Gale Moore |
Publisher | |
Pages | 174 |
Release | 1993 |
Genre | Aerodynamics |
ISBN |
This report discusses the pros and cons of numerical, semiempirical and empirical aeroprediction codes and lists many state-of-the-art codes in use today. It then summarizes many of the more popular approximate analytical methods used in State-of-the-Art (SOTA) semiempirical aeroprediction codes. It also summarizes some recent new nonlinear semiempirical methods that allow more accurate calculation of static aerodynamics on complete missile configurations to higher angles of attack. Results of static aerodynamic calculations on complete missile configurations compared to wind tunnel data are shown for several configurations at various flight conditions. Calculations show the new nonlinear methods being far superior to some of the former linear technology when used at angles of attack greater than about 15 degrees. Aeroprediction codes, Nonlinear semiempirical methods, State-of-the-Art (SOTA) semiempirical aeroprediction codes, Static aerodynamic calculations.