Aerodynamics Of Guided And Unguided Weapons

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Aerodynamics Of Guided And Unguided Weapons

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 1973

Aerodynamics Of Guided And Unguided Weapons written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Guided missiles categories.

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.

Aerodynamic Design Manual For Tactical Weapons

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Author : Lawrence Mason
language : en
Publisher:
Release Date : 1981

Aerodynamic Design Manual For Tactical Weapons written by Lawrence Mason and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with Aerodynamics categories.

Aerodynamics Of Tactical Weapons To Mach Number 3 And Angle Of Attack 15

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 1977

Aerodynamics Of Tactical Weapons To Mach Number 3 And Angle Of Attack 15 written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Angle of attack (Aerodynamics). categories.

Aerodynamics Of Tactical Weapons To Mach Number 8 And Angle Of Attack 180

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Author : Leroy Devan
language : en
Publisher:
Release Date : 1981

Aerodynamics Of Tactical Weapons To Mach Number 8 And Angle Of Attack 180 written by Leroy Devan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with Angle of attack (Aerodynamics). categories.

Computation And Comparison With Experimental Data Of The Std Arm Aerodynamic Coefficients

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Author : Frank P. Baltakis
language : en
Publisher:
Release Date : 1984

Computation And Comparison With Experimental Data Of The Std Arm Aerodynamic Coefficients written by Frank P. Baltakis and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with Aerodynamics categories.

Approximate Methods For Weapon Aerodynamics

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Author : Frankie Gale Moore
language : en
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Release Date : 2000

Approximate Methods For Weapon Aerodynamics written by Frankie Gale Moore and has been published by AIAA (American Institute of Aeronautics & Astronautics) this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with History categories.

Moore brings 30 years of experience in weapons development to help bridge the gap between the academic textbook and practical application. The book reviews all approaches to calculate aerodynamics, allowing engineers to see the pros and cons of each approach, setting the stage for a semiempirical approach. It contains many approximate aerodynamic methods, bringing together in a single text both linearized and nonlinear aerodynamic methods. Practicing engineers will value the books emphasis on understanding the physics involved, understanding the assumptions made to get to the approximate approaches, and showing final equations used in the solution process.

Improved Aeroprediction Code

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 1993

Improved Aeroprediction Code written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aerodynamic heating categories.

New 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.

The 2002 Version Of The Aeroprediction Code

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 2002

The 2002 Version Of The Aeroprediction Code written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with Aerodynamics categories.

A new version of the aeroprediction code (APC), the AP02, has been developed to address the requirements arising from advanced weapon concepts. The AP02 was formed by adding significant new technology and several productivity improvements to the previous version of the APC, the AP98. New technology added included 6 and 8 fin aerodynamics, improved nonlinear aerodynamics, improved pitch damping predictions, improved power-on base drag estimates, base-bleed effect on base drag estimation, improved axial force of nonaxisymmetric bodies and trailing-edge flap capability. Other improvements and productivity enhancements include an aerodynamic smoother, ballistic and three degree-of-freedom simulation modules as well as refinements for the pre- and post-processor for inputs and outputs of the AP02. Comparison of the predicted aerodynamics of the AP02 to AP98 and experimental data showed the AP02 to be slightly better than the AP98 in most cases that both codes would handle. However, due to the additional new technology incorporated into the AP02, many new options are available in the AP02 that are not available in the AP98. Therefore, the AP02 is more robust and, on average, is slightly more accurate than the AP98 in predicting aerodynamics of weapons.

Nonaxisymmetric Body Supersonic Aerodynamic Prediction

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Author : Leroy Devan
language : en
Publisher:
Release Date : 1987

Nonaxisymmetric Body Supersonic Aerodynamic Prediction written by Leroy Devan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Inviscid flow categories.

The 1998 Version Of The Nswc Aeroprediction Code

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 1998

The 1998 Version Of The Nswc Aeroprediction Code written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Aerodynamics categories.

The NSWC Aero prediction code has been extended to the roll position of 45 deg (fins in 'x' or cross roll orientation) in addition to the roll position of 0 deg (fins in '+' or plus roll orientation). It has also been extended to compute aerodynamics of nonaxisymmetric bodies based on an equivalent axisymmetric body. In addition, the nonlinear aerodynamic loads have been distributed over the body and lifting surfaces to provide a more useful tool for preliminary structural analysis. Finally, new technology was developed to improve the prediction of axial force at angle of attack (AOA). These new technologies have been integrated into the AP95 and will be transitioned to legitimate users as the AP98. To make the AP98 more user friendly, an upgraded pre- and post-processing, personal computer interface was also developed. Comparisons of the new theory have been made to both experimental data and the AP95. Comparisons of theory and experiment show the AP98 to be at least as good as the AP95 and, in general, maybe slightly better. In general, average accuracy levels of aerodynamics are +/- 10 percent on axial and normal force and +/- 4 percent of body length on center of pressure. For nonaxisymmetric body cases, accuracy can be slightly higher than these numbers, although not enough cases have been considered to make a definitive assessment. While these accuracy levels are encouraging for a semiempirical code, they could be improved upon by use of computational fluid dynamics codes or additional experimental data or both to reduce errors due to limited data bases.