Investigation Of The Effects Of Leading Edge Chord Extensions And Fences In Combination With Leading Edge Flaps On The Aerodynamic Characteristics At Mach Numbers From 0 40 To 0 93 Of A 45 Degree Sweptback Wing Of Aspect Ratio 4

Author : Kenneth P. Spreemann
Publisher : Unknown
Page : 644 pages
File Size : 43,6 Mb
Release : 1957
Category : Airplanes
ISBN : STANFORD:36105024832128

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Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4 by Kenneth P. Spreemann Pdf

This investigation was made to determine the effects of 6 degree full-span and 3 degree partial-span leading-edge flaps in combination with chord-extensions or fences on the aerodynamic characteristics of a wing-fuselage configuration with a 45 degree sweptback wing of aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil sections. The investigation was made in the Langley high-speed 7- by 10-foot tunnel over a Mach number range of 0.40 to 0.93 and an angle-of-attack range of about -2 degrees to 24 degrees. Lift, drag, and pitching-moment data were obtained for all configurations. From overall considerations of stability and performance it appears that with the model of this investigation the 6 degree full-span leading-edge flaps in combination with the chord-extension over the outboard 35 percent of the span, with or without leading-edge camber, would be the most desirable configuration.

Author : Kenneth P. Spreemann,William J. Alford
Publisher : Unknown
Page : 56 pages
File Size : 53,7 Mb
Release : 1957
Category : Airplanes
ISBN : UOM:39015086414482

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Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers of 0.40 to 0.93 of a 45© Sweptback Wing of Aspect Ratio 4 by Kenneth P. Spreemann,William J. Alford Pdf

Author : Alec David Young,J. H. Paterson,J. Lloyd Jones
Publisher : Unknown
Page : 159 pages
File Size : 44,5 Mb
Release : 1981
Category : Boundary layer
ISBN : 9283513924

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Aircraft Excrescence Drag by Alec David Young,J. H. Paterson,J. Lloyd Jones Pdf

Author : Harvey H. Hubbard
Publisher : Unknown
Page : 620 pages
File Size : 55,6 Mb
Release : 1991
Category : Aerodynamic noise
ISBN : STANFORD:36105024722329

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Aeroacoustics of Flight Vehicles by Harvey H. Hubbard Pdf

Author : Holt Ashley,Mårten Landahl,Marten T. Landahl
Publisher : Courier Corporation
Page : 306 pages
File Size : 52,9 Mb
Release : 1965-01-01
Category : Technology & Engineering
ISBN : 9780486648996

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Aerodynamics of Wings and Bodies by Holt Ashley,Mårten Landahl,Marten T. Landahl Pdf

This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.

Author : Edward Lewis Houghton
Publisher : Unknown
Page : 458 pages
File Size : 43,5 Mb
Release : 1978
Category : Electronic
ISBN : OCLC:916190858

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Aerodynamics for engineering students by Edward Lewis Houghton Pdf

Author : Bruce Larrimer
Publisher : Unknown
Page : 128 pages
File Size : 50,9 Mb
Release : 2020-06-15
Category : Electronic
ISBN : 1626830592

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Beyond Tube-and-Wing by Bruce Larrimer Pdf

Author : Michael E. Tauber
Publisher : Unknown
Page : 44 pages
File Size : 50,9 Mb
Release : 1989
Category : Aerodynamic heating
ISBN : UIUC:30112106607499

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A Review of High-speed, Convective, Heat-transfer Computation Methods by Michael E. Tauber Pdf

Author : Frank Hitchens
Publisher : Andrews UK Limited
Page : 877 pages
File Size : 50,9 Mb
Release : 2015-11-25
Category : Science
ISBN : 9781785383243

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The Encyclopedia of Aerodynamics by Frank Hitchens Pdf

The Encyclopedia of Aerodynamics was written for pilots at all levels from private pilot to airline pilot, military pilots and students of aerodynamics as a complete reference manual to aerodynamic terminology. General aerodynamic text books for pilots are relatively limited in their scope while aerodynamic text books for engineering students involve complex calculus. The references in this book, The Encyclopedia of Aerodynamics, are clearly described and only basic algebra is used in a few references but is completely devoid of any calculus - an advantage to many readers. Over 1400 references are included with alternative terms used where appropriate and cross-referenced throughout. The text is illustrated with 178 photographs and 96 diagrams. The Encyclopedia of Aerodynamics is an ideal aerodynamic reference manual for any pilot’s bookshelf.

Author : Donald L. Loving
Publisher : Unknown
Page : 20 pages
File Size : 42,9 Mb
Release : 1966
Category : Aerodynamic load
ISBN : UIUC:30112106686881

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Wind-tunnel-flight Correlation of Shock-induced Separated Flow by Donald L. Loving Pdf

Author : Alexander Lippisch
Publisher : Iowa State Press
Page : 144 pages
File Size : 43,7 Mb
Release : 1981
Category : Technology & Engineering
ISBN : UOM:39015026539463

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The Delta Wing by Alexander Lippisch Pdf

Den tyske flykonstruktør beskriver her udviklingen og forsøgene med Tailless- og Delta Wing- flytyper.

Author : Richard Eppler
Publisher : Springer Science & Business Media
Page : 569 pages
File Size : 47,8 Mb
Release : 2012-12-06
Category : Technology & Engineering
ISBN : 9783662026465

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Airfoil Design and Data by Richard Eppler Pdf

This 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 : Lloyd R. Jenkinson,Jim Marchman
Publisher : Elsevier
Page : 400 pages
File Size : 41,7 Mb
Release : 2003-04-28
Category : Business & Economics
ISBN : 9780080498959

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Aircraft Design Projects by Lloyd R. Jenkinson,Jim Marchman Pdf

Written 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

Author : Anonim
Publisher : Unknown
Page : 416 pages
File Size : 55,8 Mb
Release : 1982
Category : Aerodynamics
ISBN : 9283503228

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High Angle-of-attack Aerodynamics by Anonim Pdf

Author : Hermann Schlichting,Erich Truckenbrodt
Publisher : McGraw-Hill Companies
Page : 560 pages
File Size : 50,9 Mb
Release : 1979
Category : Science
ISBN : STANFORD:36105030529981

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Aerodynamics of the Airplane by Hermann Schlichting,Erich Truckenbrodt Pdf