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Effects Of Wing Modification On An Aircrafts Aerodynamic Parameters As Determined From Flight Data
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Book Synopsis Effects of Wing Modification on an Aircraft's Aerodynamic Parameters as Determined from Flight Data by : Robert Alan Hess
Download or read book Effects of Wing Modification on an Aircraft's Aerodynamic Parameters as Determined from Flight Data written by Robert Alan Hess and published by . This book was released on 1986 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-wing Airplane Model by : Charles L. Seacord
Download or read book Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-wing Airplane Model written by Charles L. Seacord and published by . This book was released on 1945 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: An investigation of the power-off longitudinal stability characteristics of a tailless all-wing airplane model with various wing modifications has been made in the Langley free-flight tunnel. Force and tuft tests were made on the model in the original condition, with the wing tips rotated for washout, with rectangular and swept-forward tips, and with various slat arrangements. Flight tests were made with the original wing and with the original wing equipped with the most promising modifications. The results indicated that changes in tip plan form or rotation of the wing tips did not appreciably reduce the instability at high lift coefficients. Addition of wing slats, however, improved the longitudinal stability at the stall when the slat extended far enough inboard to cover the area that tended to stall first.
Book Synopsis Introductory Aerodynamics and Hydrodynamics of Wings and Bodies by : Frederick O. Smetana
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 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt: Annotation 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. The text 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 determine easily 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.
Book Synopsis Effects of Wing and Nacelle Modifications on Drag and Wake Characteristics of a Bomber-type Airplane Model by : Robert H. Neely
Download or read book Effects of Wing and Nacelle Modifications on Drag and Wake Characteristics of a Bomber-type Airplane Model written by Robert H. Neely and published by . This book was released on 1945 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: An investigation of a model of a large four-engine bomber was conducted in the Langley 19-foot pressure tunnel to determine the effects of several wing and nacelle modification on drag characteristics and air-flow characteristics at the tail. Leading-edge gloves, trailing-edge extensions, and modified nacelle afterbodies were tested individually and in combination. The effects of the various modifications were determined by force tests, tuft observations, and turbulence surveys in the region of the tail. Tests were made with fixed and natural transition on the wing and with propellers operating and propellers off. Most of the tests were conducted at a Reynolds number of approximately 2.6 x 106. The results indicated that application of certain of the modifications provided worth-while improvements in the characteristics of the model. The flow over the wing and flaps was improved, the drag was reduced, and the turbulence in the region of the tail was reduced.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing-leading-edge Modifications on a Full-scale, Low-wing General Aviation Airplane: Wind-tunnel Investigation of High-angle-of-attack Aerodynamic Characteristics by : William A. Jr Newson
Download or read book Effects of Wing-leading-edge Modifications on a Full-scale, Low-wing General Aviation Airplane: Wind-tunnel Investigation of High-angle-of-attack Aerodynamic Characteristics written by William A. Jr Newson and published by . This book was released on 1982 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing-leading-edge Modifications on a Full-scale, Low-wing General Aviation Airplane by : William A. Newsom
Download or read book Effects of Wing-leading-edge Modifications on a Full-scale, Low-wing General Aviation Airplane written by William A. Newsom and published by . This book was released on 1982 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Langley Research Center. Research Information and Applications Division Publisher : ISBN 13 : Total Pages :270 pages Book Rating :4.:/5 (317 download)
Book Synopsis Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986 by : Langley Research Center. Research Information and Applications Division
Download or read book Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986 written by Langley Research Center. Research Information and Applications Division and published by . This book was released on 1987 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Introduction to Aircraft Flight Mechanics by : Thomas R. Yechout
Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based 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.
Book Synopsis The High-speed Aerodynamic Effects of Modifications to the Wing and Wing-fuselage Intersection of an Airplane Model with the Wing Swept Back 35 Degrees by : Lee E. Boddy
Download or read book The High-speed Aerodynamic Effects of Modifications to the Wing and Wing-fuselage Intersection of an Airplane Model with the Wing Swept Back 35 Degrees written by Lee E. Boddy and published by . This book was released on 1948 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Modeling of Aircraft Unsteady Aerodynamic Characteristics/Part 3 - Parameters Estimated from Flight Data by :
Download or read book Modeling of Aircraft Unsteady Aerodynamic Characteristics/Part 3 - Parameters Estimated from Flight Data written by and published by . This book was released on 1996 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scale Effects on Aircraft and Weapon Aerodynamics by : A. B. Haines
Download or read book Scale Effects on Aircraft and Weapon Aerodynamics written by A. B. Haines and published by . This book was released on 1994 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1971 with total page 1388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1976 with total page 1408 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87 by : Royce L. McKinney
Download or read book Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87 written by Royce L. McKinney and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1948 with total page 446 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index by :
Download or read book Government Reports Annual Index written by and published by . This book was released on 1986 with total page 872 pages. Available in PDF, EPUB and Kindle. Book excerpt:
