rdf-syntax-grammar
mods:
  schema location: http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
  title info:
    title: Wing theory in supersonic flow
  name:
    name part: Carafoli, Elie.
    role:
      role term: creator
  name:
    name part: Mateescu, Dan
    role:
      role term: author.
  name:
    name part: Năstase, Adriana
    role:
      role term: author.
  name:
    name part: ScienceDirect (Online service)
  type of resource: text
  genre: bibliography
  genre: Electronic books.
  origin info:
    place:
      place term: enk
    place:
      place term: Oxford
    place:
      place term: New York
    publisher: Pergamon Press
    date issued: [1969]
    date issued: 1969
    edition: [1st ed.].
    issuance: monographic
  language:
    language term: eng
  physical description:
    reformatting quality: access
    form: remote
    extent: 1 online resource (xiii, 594 pages)
  abstract: Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more complex system. Organized into 12 chapters, this volume starts with an overview of the basic equations in the mechanics of inviscid fluids. This text then presents a unified theory that is established for angularly shaped wings in supersonic flow. Other chapters consider the method for calculating the.
  table of contents: Front Cover; Wing Theory in Supersonic Flow; Copyright Page; Table of Contents; PREFACE; ACKNOWLEDGEMENTS; CHAPTER I. RECAPITULATIVE SURVEY OF THE EQUATIONS OF MOTIONOF PERFECT FLUIDS IN SUPERSONIC FLOW; I. 1. General Equations; I. 2. Propagation of Small Disturbances; I. 3. Velocity Potential Equation; I. 4. Pressure Coefficient under the Assumption of Small Disturbances; I. 5. Theory of Wings of Infinite Aspect Ratio in Supersonic Flow underthe Assumption of Small Disturbances.
  table of contents: I. 6. Theory of Axially-symmetric Bodies under the Assumption of SmallDisturbances (Application to the Circular Cone)I. 7. Conical Motions in Supersonic Flow; I. 8. High-order Conical Flows; CHAPTER II. UNIFIED THEORY OF ANGULAR WINGS BASED ON HIGH-ORDERCONICAL FLOW DETERMINATION OF THE AXIAL DISTURBANCE VELOCITY(u) AND OF THE DOWNWASH (w) IN THE DIRECT, INDIRECT ANDMIXED PROBLEMS; II. 1. General Considerations; CHAPTERIII. THE CALCULATION OF THE OVERALL FORCES AND MOMENTS ONWINGS WITH TRAILING EDGES OF ARBITRARY PLANFORM SHAPE.
  table of contents: II. 2. Behaviour of the Axial Disturbance Velocity u in the Neighbourhoodof the Subsonic Leading Edges or the Subsonic Ridges on the ThinWing (Direct Problem)II. 3. Contribution of the Subsonic Leading Edges of Thin Wings and of the Separation Ridges to the Construction of the Velocity u (DirectProblem); II. 4. Examples of Application to Ordinary Wings in the Direct Problem; II. 5. Determination of Constants; II. 6. Examples of the Determination of Constants.
  table of contents: II. 7. Contribution of the Ridges and the Leading Edge to the Calculation ofthe Downwash w, when the Pressures are given on the Wing(Indirect Problem)II. 8. Some Considerations on the Indirect Problem; II. 9. Wing whose Incidence Variation and Pressure Distribution are givenAlternatively on Separate Portions (Mixed Problem); III. 1. Preliminary Considerations; III. 2. Calculation of Forces; III. 3. Calculation of Moments; III. 4. Some Special Applications of the Formulae for Calculating the Forcesand Moments.
  table of contents: III. 5. Calculation of the Suction Force induced by the Subsonic LeadingEdges of a Thin WingCHAPTERIV. STUDY OF ORDINARY DELTA WINGS; IV. 1. Introductory Considerations on the Delta Wing; IV. 2. Thin Delta Wing with Subsonic Leading Edges having SymmetricalIncidences; IV. 3. Thin Delta Wing with Subsonic Edges having Antisymmetrical Incidences; IV. 4. Thin Delta Wing with Supersonic Edges and Symmetry of Incidence; IV. 5. Wing of Symmetrical Thickness; IV. 6. Thin Delta Wing with Supersonic Edges and Antisymmetry of Incidence; IV. 7. Delta Wing with Sonic Leading Edges.
  note: by Elie Carafoli ; with the cooperation of Dan Mateescu and Adriana Nastase.
  note: Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. http://purl.oclc.org/DLF/benchrepro0212 MiAaHDL
  note: digitized 2010 HathiTrust Digital Library committed to preserve pda MiAaHDL
  note: Includes bibliographical references (pages 565-588).
  note: English.
  subject:
    topic: Aerodynamics, Supersonic
  subject:
    topic: Airplanes
    topic: Wings
  subject:
    topic: Aérodynamique supersonique
  subject:
    topic: Avions
    topic: Ailes
  subject:
    topic: TECHNOLOGY & ENGINEERING
    topic: Engineering (General)
  subject:
    topic: Aerodynamics, Supersonic
  subject:
    topic: Airplanes
    topic: Wings
  subject:
    topic: Bemessungsgrundlage
  subject:
    topic: Berechnung
  subject:
    topic: Deltaflügel
  subject:
    topic: Überschallströmung
  subject:
    topic: Aeroplanes
    topic: Wings
  classification: TL672 .C3 1969
  classification: 629.13432
  related item:
    title info:
      title: Wing theory in supersonic flow
    name:
      name part: Carafoli, Elie.
    origin info:
      publisher: Oxford, New York, Pergamon Press [1969]
      edition: [1st ed.].
    identifier: (DLC) 67027481
    identifier: (OCoLC)180754
  related item:
    title info:
      title: International series of monographs in aeronautics and astronautics. v. 7
      part number: Division 2
      part name: Aerodynamics
  identifier: 9781483160276
  identifier: 1483160270
  identifier: 0080123309
  identifier: 9780080123301
  identifier: http://proxy.library.tamu.edu/login
  record info:
    record content source: OCLCE
    record creation date: 100423
    record change date: 20260326174125.9
    record identifier: in00005742089
    language of cataloging:
      language term: eng