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  • 1
    Book
    Book
    Amsterdam u.a. : North-Holland
    UID:
    b3kat_BV009220764
    Format: VIII, 473 S. , graph. Darst.
    ISBN: 0444879587
    Series Statement: North-Holland series in applied mathematics and mechanics 30
    Language: English
    Subjects: Physics
    RVK:
    Keywords: Transsonische Strömung ; Aerodynamik
    Library Location Call Number Volume/Issue/Year Availability
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  • 2
    Book
    Book
    Amsterdam [u.a.] : North-Holland
    UID:
    gbv_272715255
    Format: VIII, 473 S. , graph. Darst.
    ISBN: 0444879587
    Series Statement: North Holland series in applied mathematics and mechanics 30
    Note: Literaturangaben , Front Cover; Transonic Aerodynamics; Copyright Page; Dedication; Table of Contents; Chapter 1. Introduction; 1.1 Framework; 1.2 Mathematics; 1.3 Historical Note; Chapter 2. Linearized Theory - Transonic Breakdown; 2.1 Equations of Acoustics; 2.2 Galilean Transformation - Uniform Translation; 2.3 Slender Body Theory - Acoustics; 2.4 Exact Equations of Planar Flow; Shock Waves and Entropy Jump; 2.5 Linearized Theory for Thin Airfoils; Chapter 3. Transonic Expansion Procedures; Simple Solutions, Integral Relations; 3.1 Expansion Procedure For Steady Flow Past Airfoils. - 3.2 Expansion Procedure Applied to the Basic System of Equations3.3 Expansion Procedures for Jet Flows; 3.4 Transonic Similarity Rules; 3.5 Hodograph Equations for Planar Flow; 3.6 Simple Waves, Shock Waves, Detachment; 3.7 Nozzle Flow, Branch Lines, Limit Lines; 3.8 Subsonic and Sonic Jets; 3.9 Transonic Slender Bodies: Expansion Procedure, Area Rule; 3.10 Lift and Drag Integrals; 3.11 Unsteady Transonic Flow; Chapter 4. Transonic Far Fields; 4.1 Far Field at M = 1 (K =0); 4.2 Far Field at M〉 1; 4.3 Far Fields at M 0); References; Chapter 5. Transonic Airfoil Theory. - 5.1 Problem Formulation5.2 Nose Singularity; 5.3 Shock Wave at a Curved Surface; 5.4 Numerical Methods, Physical Plane, Steady Flow; 5.5 Airfoils at Sonic Velocity; 5.6 The Stabilization Law; Chapter 6. Three Dimensional Wings; 6.1 Unswept Wings, M 〈 1; 6.2 Swept Wings M 〈 1; 6.3 Unswept Wings, M = 1; Chapter 7. Quasi-transonic Flow; 7.1 Linearized Theory; 7.2 Quasi-transonic Equations; 7.3 Application to Delta Wing with Wedge Cross - Section; 7.4 Remarks; Index
    Language: English
    Subjects: Physics
    RVK:
    Keywords: Transsonische Strömung
    Library Location Call Number Volume/Issue/Year Availability
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