Aerodynamics of Tactical Weapons to Mach Number 3 and Angle of Attack 15
Author: Roy C. Swanson (Jr.)
Publisher:
Published: 1977
Total Pages: 192
ISBN-13:
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Author: Roy C. Swanson (Jr.)
Publisher:
Published: 1977
Total Pages: 192
ISBN-13:
DOWNLOAD EBOOKAuthor: Leroy Devan
Publisher:
Published: 1981
Total Pages: 348
ISBN-13:
DOWNLOAD EBOOKAuthor: Frank G. Moore
Publisher:
Published: 1977
Total Pages:
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DOWNLOAD EBOOKAuthor: Frankie Gale Moore
Publisher:
Published: 1993
Total Pages: 174
ISBN-13:
DOWNLOAD EBOOKThis 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.
Author: Frankie Gale Moore
Publisher:
Published: 1993
Total Pages: 168
ISBN-13:
DOWNLOAD EBOOKNew and improved version of the Naval Surface Warfare Center, Dahlgren Division aeroprediction code (AP93) has been developed. The new code contains new technology that allows planar aerodynamics of axisymmetric solid rocket-type weapons to be computed with engineering accurately over the entire Mach number range and for angles of attack to 30 deg. New technology developed and included in the AP93 includes; A new engineering method to compute aeroheating information at a high Mach number; Extension of the second-order shock-expansion theory to include real-gas effects, including several new pressure prediction techniques; An improved body-alone nonlinear normal-force method; New methods for computing nonlinear aerodynamics of wing alone, wing body, and body wing due to angle of attack, and wing body due to control deflection; and a new base-dmg database and improved empirical base-drag estimation technique. ... Aeroprediction code (AP93), Planar aerodynamics, High mach number.
Author: Lawrence Mason
Publisher:
Published: 1981
Total Pages: 182
ISBN-13:
DOWNLOAD EBOOKAuthor: Naval Surface Warfare Center (U.S.). Dahlgren Division
Publisher:
Published: 1998
Total Pages: 180
ISBN-13:
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Publisher:
Published: 1980-11
Total Pages: 418
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Publisher:
Published: 1989
Total Pages: 1134
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DOWNLOAD EBOOKAuthor: Donald W. Ausherman
Publisher:
Published: 1992
Total Pages: 190
ISBN-13:
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