Download or read book Development of a Computer Program to Calculate Aerodynamic Characteristics of Bodies and Wing body Combinations written by Fred R. DeJarnette and published by . This book was released on 1978 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new method has been developed for calculating an approximate surface pressure distribution over axisymmetric bodies, with pointed or blunted noses, at angle of attack in supersonic flow. A modified form of the second-order shock-expansion method is developed and matched to modified Newtonian theory near the nose. Surface pressure distributions compared well with experimental data on blunted cones with and without flares at Mach numbers from 1.5 to 4.63 and angles of attack to 12°.

Download or read book Development of a Computer Program to Calculate Aerodynamic Characteristics of Bodies and Wing Body Combinations written by and published by . This book was released on 1978 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new method has been developed for calculating an approximate surface pressure distribution over axisymmetric bodies, with pointed or blunted noses, at angle of attack in supersonic flow. A modified form of the second-order shock-expansion method is developed and matched to modifed Newtonian theory near the nose. Surface pressure distributions compared well with experimental data on blunted cones with and without flares at Mach numbers from 1.5 to 4.63 and angles of attack to 12 deg. (Author).

Download or read book Development of a Computer Program to Calculate Aerodynamic Characteristics of Bodies at Supersonic Mach Numbers written by Kenneth Morris Jones and published by . This book was released on 1978 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book State of the art Engineering Aeroprediction Methods with Emphasis on New Semiempirical Techniques for Predicting Nonlinear Aerodynamics on Complete Missile Configurations written by Frankie Gale Moore and published by . This book was released on 1993 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Download or read book A Computer Program for Calculating Symmetrical Aerodynamic Characteristics and Lateral directional Stability Derivatives of Wing body Combinations with Blowing Jets written by and published by . This book was released on 1978 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1972 with total page 1056 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1989 with total page 1148 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Computer Program for the Prediction of Aerodynamic Characteristics of Wing body tail Combinations at Subsonic and Supersonic Speeds written by S. Anders and published by . This book was released on 1972 with total page 119 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Development of an Empirically Based Computer Program to Predict the Aerodynamic Characteristics of Aircraft written by Roy T. Schemensky and published by . This book was released on 1973 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1982 with total page 964 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aeronautical Engineering written by and published by . This book was released on 1991 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book COSMIC Software Catalog written by and published by . This book was released on 1987 with total page 444 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Monthly Catalogue United States Public Documents written by and published by . This book was released on 1982 with total page 1102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Computer Programs for Calculating the Static Longitudinal Aerodynamic Characteristics of Wing body tail Cinfigurations written by Michael R. Mendenhall and published by . This book was released on 1975 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Computer Programs for Calculating the Static Longitudinal Aerodynamic Characteristics of Wing body tail Configurations written by and published by . This book was released on 1975 with total page 230 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Introductory Aerodynamics and Hydrodynamics of Wings and Bodies written by Frederick O. Smetana and published by Aiaa. This book was released on 1997-01-01 with total page 241 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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. "Introductory Aerodynamics and Hydrodynamics of Wings and Bodies: A Software-Based Approach" 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 easily determine 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. System Requirements: IBM 386 (compatible) or higher, MS DOS 6.x, Windows 3.11, 8 Mb RAM

Download or read book A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback wing body Combination Designed for High Performance written by Donald L. Loving and published by . This book was released on 1961 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: