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

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

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Author : Roy C. Swanson (Jr.)
language : en
Publisher:
Release Date : 1977

Aerodynamics Of Tactical Weapons To Mach Number 3 And Angle Of Attack 15 written by Roy C. Swanson (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 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 : 1980

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 1980 with Angle of attack (Aerodynamics). categories.

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

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Author : Frank G. Moore
language : en
Publisher:
Release Date : 1977

Aerodynamics Of Tactical Weapons To Mach Number 3 Angle Of Attack 15 Deg written by Frank G. 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 categories.

Technical Digest

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Author : Naval Surface Warfare Center (U.S.). Dahlgren Division
language : en
Publisher:
Release Date : 1998

Technical Digest written by Naval Surface Warfare Center (U.S.). Dahlgren Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Naval research categories.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1989

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Aeronautics categories.

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.

Surface Pressure Measurements On A Double Delta Wing Body Configuration At Mach 2 And Mach 3 Wtr 1396

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Author : Donald W. Ausherman
language : en
Publisher:
Release Date : 1992

Surface Pressure Measurements On A Double Delta Wing Body Configuration At Mach 2 And Mach 3 Wtr 1396 written by Donald W. Ausherman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Angle of attack (Aerodynamics). 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.

Drag Predictions For Projectiles At Transonic And Supersonic Speeds

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Author : Jubaraj Sahu
language : en
Publisher:
Release Date : 1986

Drag Predictions For Projectiles At Transonic And Supersonic Speeds written by Jubaraj Sahu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with Drag (Aerodynamics) categories.

The breakdown of the total drag into its individual components (pressure drag, viscous drag, and base drag) is important in the preliminary design stage of shell. Design codes are available to predict the individual drag components and thus, the total drag. Typically, the total drag predicted by these design codes agrees well with the total drag measured from flight tests. But, how well do these codes predict the individual drag components? Experimental verification of the prediction of the drag components is an extremely difficult task. Thus a Navier-Stokes computational procedure is used in this report to predict the individual drag components and test the accuracy of the predictions of the design codes. A thin-layer Navier-Stokes code has been used to compute the entire flow field over projectiles including the base region. Numerical calculations have been made for various Mach numbers in the transonic and supersonic regimes. Pressure drag, skin friction drag, base drag and thus, the total drag are obtained from the computed results. Comparison of drag has been made with available experimental data and also with predictions from design codes employing semi-empirical techniques.