Improved Curve Fits for the Thermodynamic Properties of Equilibrium Air Suitable for Numerical Computation Using Time-dependent Or Shock-capturing Methods PDF Download
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Author: John C. Tannehill
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 44
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Book Description
Author: John C. Tannehill
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 44
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 250
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Book Description
Author: Supramaniam Srinivasan
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 56
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Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 672
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Book Description
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 268
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Book Description
Author: Frankie Gale Moore
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 168
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Book Description
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.
Author: Supramaniam Srinivasan
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 58
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Book Description
Author: A. J. Baker
Publisher: John Wiley & Sons
ISBN: 1119940494
Category : Technology & Engineering
Languages : en
Pages : 574
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Book Description
Covers the theory and applications of using weak form theory in incompressible fluid-thermal sciences Giving you a solid foundation on the Galerkin finite-element method (FEM), this book promotes the use of optimal modified continuous Galerkin weak form theory to generate discrete approximate solutions to incompressible-thermal Navier-Stokes equations. The book covers the topic comprehensively by introducing formulations, theory and implementation of FEM and various flow formulations. The author first introduces concepts, terminology and methodology related to the topic before covering topics including aerodynamics; the Navier-Stokes Equations; vector field theory implementations and large eddy simulation formulations. Introduces and addresses many different flow models (Navier-Stokes, full-potential, potential, compressible/incompressible) from a unified perspective Focuses on Galerkin methods for CFD beneficial for engineering graduate students and engineering professionals Accompanied by a website with sample applications of the algorithms and example problems and solutions This approach is useful for graduate students in various engineering fields and as well as professional engineers.
Author: Frankie Gale Moore
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 174
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Book Description
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.
Author: Donald W. Ausherman
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics).
Languages : en
Pages : 190
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Book Description
