Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61
Author: Emma Jean Landrum
Publisher:
Published: 1960
Total Pages: 70
ISBN-13:
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Author: Emma Jean Landrum
Publisher:
Published: 1960
Total Pages: 70
ISBN-13:
DOWNLOAD EBOOKAuthor: Thomas R. Yechout
Publisher: AIAA
Published: 2003
Total Pages: 666
ISBN-13: 9781600860782
DOWNLOAD EBOOKBased on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author: Robert C. Nelson
Publisher:
Published: 1998
Total Pages: 464
ISBN-13:
DOWNLOAD EBOOKThis edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author: Douglas R. Lord
Publisher:
Published: 1957
Total Pages: 52
ISBN-13:
DOWNLOAD EBOOKAn investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01 to determine the aerodynamic characteristics of a spoiler-slot-deflector control on a 45 degree sweptback wing having an aspect ratio of 3.5, a taper ratio of 0.3, and an NACA 65A005 airfoil section. The model was equipped with a 15-percent-chord spoiler-slot-deflector extending from 13 o 78 percent of the wing semispan. The spoiler and deflector were hinged along the 60- and 75-percent-chord lines, respectively. Tests were made at a Reynolds number of 3,000,000 (based on the mean aerodynamic chord of the wing) and covered ranges of angles of attack from -3 to 15 degrees, spoiler projections from 0 to 8.0 percent chord, and deflector projections from 0 to 7.6 percent chord.
Author: Richard Eppler
Publisher: Springer Science & Business Media
Published: 2012-12-06
Total Pages: 569
ISBN-13: 3662026465
DOWNLOAD EBOOKThis detailed book describes a procedure for the design and analysis of subsonic airfoils. Contains 116 new airfoils for a wide range of Reynolds numbers and application requirements, including the input data for the computer code.
Author: Ira H. Abbott
Publisher: Courier Corporation
Published: 2012-04-26
Total Pages: 708
ISBN-13: 0486134997
DOWNLOAD EBOOKConcise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.
Author: Richard Shepherd Shevell
Publisher: Pearson Education India
Published: 1989
Total Pages: 468
ISBN-13: 9788177587425
DOWNLOAD EBOOKAuthor: Bernard Etkin
Publisher: John Wiley & Sons
Published: 1982
Total Pages: 392
ISBN-13:
DOWNLOAD EBOOKAuthor: Barnes Warnock McCormick
Publisher: Courier Corporation
Published: 1999-01-01
Total Pages: 356
ISBN-13: 9780486404608
DOWNLOAD EBOOKAn extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.
Author: Lloyd R. Jenkinson
Publisher: Elsevier
Published: 2003-04-28
Total Pages: 393
ISBN-13: 0080498957
DOWNLOAD EBOOKWritten with students of aerospace or aeronautical engineering firmly in mind, this is a practical and wide-ranging book that draws together the various theoretical elements of aircraft design - structures, aerodynamics, propulsion, control and others - and guides the reader in applying them in practice. Based on a range of detailed real-life aircraft design projects, including military training, commercial and concept aircraft, the experienced UK and US based authors present engineering students with an essential toolkit and reference to support their own project work.All aircraft projects are unique and it is impossible to provide a template for the work involved in the design process. However, with the knowledge of the steps in the initial design process and of previous experience from similar projects, students will be freer to concentrate on the innovative and analytical aspects of their course project. The authors bring a unique combination of perspectives and experience to this text. It reflects both British and American academic practices in teaching aircraft design. Lloyd Jenkinson has taught aircraft design at both Loughborough and Southampton universities in the UK and Jim Marchman has taught both aircraft and spacecraft design at Virginia Tech in the US.* Demonstrates how basic aircraft design processes can be successfully applied in reality* Case studies allow both student and instructor to examine particular design challenges * Covers commercial and successful student design projects, and includes over 200 high quality illustrations