Mathematical Methods in Defense Analyses

Mathematical Methods in Defense Analyses
Author: J. S. Przemieniecki
Publisher: AIAA
Total Pages: 434
Release: 2000
Genre: Military art and science
ISBN: 9781600860850

Annotation This text presents the various mathematical methods used in military operations research in one easy-to-use reference volume. The reader will find the calculations necessary to analyze all aspects of defense operations, from weapon performance to combat modeling. The text is so clearly written and organized that even newcomers to the field will find it useful. Included with the text is an updated version of Defense Analyses Software, a compendium of software subroutines that allow the reader to compute numerical values for functions or tables derived in the text. Each subroutine is provided with a detailed reference to the equation from which it was derived to ensure that its intended application is consistent with the assumptions used in the derivation. The third edition has a new chapter on theater missile defense based on the concept of layered defense with different strategies of allocating defense interceptors against short- or mid-range ballistic missiles.

Introductory Aerodynamics and Hydrodynamics of Wings and Bodies

Introductory Aerodynamics and Hydrodynamics of Wings and Bodies
Author: Frederick O. Smetana
Publisher: AIAA
Total Pages: 270
Release: 1997
Genre: Aerodynamics
ISBN: 9781600860836

Annotation This textbook and its six supporting computer programs provide theoretical modeling of the aerodynamic characteristics of wings and bodies at low Mach numbers. The approach presented directly helps engineering students improve problem-solving skills by teaching them to discern the necessary steps associated with solving analytical problems. The book also presents a justification and rationale for validating end results that leave the student with an understanding of the answer. The text differs from others by providing interactive computer programs that allow the student to conduct trade studies. It provides case-specific software that permits the student to do considerably more characteristic analysis of user-selected wings and bodies than is possible with other introductory textbooks. In addition, the algorithms are capable of working problems at a level well beyond those typically solved by hand in other textbooks. This approach allows students to determine easily the effects of modifying parameters and geometry. Another benefit of using this textbook is the understanding students gain of the capabilities of large industrial codes.

1994 NASA Authorization

1994 NASA Authorization
Author: United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation
Publisher:
Total Pages: 232
Release: 1993
Genre:
ISBN: