Maximum Lift-drag Ratios of Delta-wing
Author: Patrick J. Johnston
Publisher:
Published: 1965
Total Pages: 26
ISBN-13:
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Author: Patrick J. Johnston
Publisher:
Published: 1965
Total Pages: 26
ISBN-13:
DOWNLOAD EBOOKAuthor: David E. Fetterman
Publisher:
Published: 1963
Total Pages: 72
ISBN-13:
DOWNLOAD EBOOKAuthor: Barnes W. McCormick
Publisher: John Wiley & Sons
Published: 1994-09-28
Total Pages: 677
ISBN-13: 0471575062
DOWNLOAD EBOOKA New Edition of the Most Effective Text/Reference in the Field! Aerodynamics, Aeronautics, and Flight Mechanics, Second Edition Barnes W. McCormick, Pennsylvania State University 57506-2 When the first edition of Aerodynamics, Aeronautics, and Flight Mechanics was published, it quickly became one of the most important teaching and reference tools in the field. Not only did generations of students learn from it, they continue to use it on the job-the first edition remains one of the most well-thumbed guides you'll find in an airplane company. Now this classic text/reference is available in a bold new edition. All new material and the interweaving of the computer throughout make the Second Edition even more practical and current than before! A New Edition as Complete and Applied as the First Both analytical and applied in nature, Aerodynamics, Aeronautics, and Flight Mechanics presents all necessary derivations to understand basic principles and then applies this material to specific examples. You'll find complete coverage of the full range of topics, from aerodynamics to propulsion to performance to stability and control. Plus, the new Second Edition boasts the same careful integration of concepts that was an acclaimed feature of the previous edition. For example, Chapters 9, 10, and 11 give a fully integrated presentation of static, dynamic, and automatic stability and control. These three chapters form the basis of a complete course on stability and control. New Features You'll Find in the Second Edition * A new chapter on helicopter and V/STOL aircraft- introduces a phase of aerodynamics not covered in most current texts * Even more material than the previous edition, including coverage of stealth airplanes and delta wings * Extensive use of the computer throughout- each chapter now contains several computer exercises * A computer disk with programs written by the author is available
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1958
Total Pages: 678
ISBN-13:
DOWNLOAD EBOOKAuthor: Robert W. Dunning
Publisher:
Published: 1953
Total Pages: 24
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1958
Total Pages: 658
ISBN-13:
DOWNLOAD EBOOKAuthor: Robert L. Trimpi
Publisher:
Published: 1958
Total Pages: 682
ISBN-13:
DOWNLOAD EBOOKThe linearized attenuation theory of NACA Technical Note 3375 is modified in the following manner: (a) an unsteady compressible local skin-friction coefficient is employed rather than the equivalent steady-flow incompressible coefficient; (b) a nonlinear approach is used to permit application of the theory to large attenuations; and (c) transition effects are considered. Curves are presented for predicting attenuation for shock pressure ratios up to 20 and a range of shock-tube Reynolds numbers. Comparison of theory and experimental data for shock wave strengths between 1.5 and 10 over a wide range of Reynolds numbers shows good agreement with the nonlinear theory evaluated for a transition Reynolds nuniber of 2.5 million.
Author: William J. Small
Publisher:
Published: 1966
Total Pages: 66
ISBN-13:
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