Fin Loads and Tip-control Hinge Moments on a 1/8-scale Model Simulating the First Stage of the Scout Research Vehicle at a Mach Number of 2.01
Author: Ross B. Robinson
Publisher:
Published: 1960
Total Pages: 22
ISBN-13:
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Author: Ross B. Robinson
Publisher:
Published: 1960
Total Pages: 22
ISBN-13:
DOWNLOAD EBOOKAuthor: Ming H. Tang
Publisher:
Published: 1971
Total Pages: 52
ISBN-13:
DOWNLOAD EBOOKAuthor: Byron M. Jaquet
Publisher:
Published: 1963
Total Pages: 64
ISBN-13:
DOWNLOAD EBOOKAuthor: Joseph R. Chambers
Publisher: NASA
Published: 2014
Total Pages: 533
ISBN-13: 9781626830165
DOWNLOAD EBOOKAuthor: James D. Church
Publisher:
Published: 1954
Total Pages: 30
ISBN-13:
DOWNLOAD EBOOKA free-flight investigation has been conducted to determine normal-force and hinge-moment characteristics of a half-diamond tip control on a diamond wing having 60 degree sweptback leading edges and 30 degree sweptforward trailing edges through a range of Mach number of 0.5 to 1.3. Results indicate that the control could be so hinged that very small hinge-moments due to control deflection would be obtained at low angles of attack over the speed range tested, although nonlinear variations of hinge moment with angle of attack were present in the transonic range.
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
Published: 2018-09-10
Total Pages: 28
ISBN-13: 9781720213932
DOWNLOAD EBOOKThe hinge moments, at selected flight conditions, resulting from deflecting two trailing edge control surfaces (one inboard and one midspan) on a high aspect ratio, swept, fuel conservative wing with a supercritical airfoil are estimated. Hinge moment results obtained from procedures which employ a recently developed transonic analysis are given. In this procedure a three dimensional inviscid transonic aerodynamics computer program is combined with a two dimensional turbulent boundary layer program in order to obtain an interacted solution. These results indicate that trends of the estimated hinge moment as a function of deflection angle are similar to those from experimental hinge moment measurements made on wind tunnel models with swept supercritical wings tested at similar values of free stream Mach number and angle of attack. Perry, B., III Langley Research Center NASA-TM-78664, L-12219 RTOP 516-53-03-21
Author: Robert J. Keynton
Publisher:
Published: 1971
Total Pages: 52
ISBN-13:
DOWNLOAD EBOOKAuthor: Richard Shepherd Shevell
Publisher: Pearson Education India
Published: 1989
Total Pages: 468
ISBN-13: 9788177587425
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: Richard P. Hallion
Publisher:
Published: 1984
Total Pages: 420
ISBN-13:
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