Library

feed icon rss

Your email was sent successfully. Check your inbox.

An error occurred while sending the email. Please try again.

Proceed reservation?

Export
  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Fluid dynamics 23 (1988), S. 325-333 
    ISSN: 1573-8507
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Notes: Abstract A mathematically rigorous approach to the solution of inverse boundary-value problems of aerohydrodynamics — problems in which the airfoil contour is found from the given distribution of the velocity as a function of the arc abscissa – is proposed. The approach is based on the notion of a quasisolution in the theory of improperly posed problems and involves a controlled modification of the initial data for the purpose of obtaining a unique solution in a given class of contours. The approach is explained with reference to the problem of designing an isolated airfoil in a plane steady ideal incompressible flow and is extended to the cases of subsonic gas flow and viscous incompressible flow. Some numerical results illustrating the possibilities of the method are also presented.
    Type of Medium: Electronic Resource
    Library Location Call Number Volume/Issue/Year Availability
    BibTip Others were also interested in ...
  • 2
    Electronic Resource
    Electronic Resource
    Springer
    Fluid dynamics 12 (1977), S. 210-217 
    ISSN: 1573-8507
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Notes: Abstract The stability of the solutions of a group of problems regarding the construction of an underground contour on the basis of the distribution of filtration pressure is considered for bounded and unbounded depths of the water-permeable layer and also for the case of an inclined water-resistant boundary.
    Type of Medium: Electronic Resource
    Library Location Call Number Volume/Issue/Year Availability
    BibTip Others were also interested in ...
  • 3
    Electronic Resource
    Electronic Resource
    Springer
    Fluid dynamics 27 (1992), S. 423-428 
    ISSN: 1573-8507
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Notes: Abstract Within the framework of Chapygin's approximate method the problem of maximizing M∞ for a selected class of lifting airfoils is reduced to a minimax problem of special type. An exact solution of the latter problem is constructed for an expanded class of flows, including multivalent flows. Profiles with a higher than normal critical Mach number are indicated.
    Type of Medium: Electronic Resource
    Library Location Call Number Volume/Issue/Year Availability
    BibTip Others were also interested in ...
  • 4
    Electronic Resource
    Electronic Resource
    Springer
    Fluid dynamics 25 (1990), S. 462-469 
    ISSN: 1573-8507
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Notes: Abstract A general formulation of the inverse boundary-value problem of aerohydrodynamics for v(s) is given for two angles of attack. This formulation includes that given in [10] as a particular case. An integral representation of the solution is constructed, and the conditions of consistency of the initial data and the solvability conditions are written down. For satisfying the latter the method of quasisolutions of inverse boundary-value problems [11, 12] is employed. A criterion is obtained for the absence of boundary layer separation as the angle of attack varies over a given range. This criterion is expressed in terms of the velocity distributions for the limiting positions. A method of specifying hydrodynamically expedient velocity distributions that takes into account the nonstalling conditions obtained is proposed. Questions of lift maximization are considered. The results of numerical calculations are presented.
    Type of Medium: Electronic Resource
    Library Location Call Number Volume/Issue/Year Availability
    BibTip Others were also interested in ...
  • 5
    Electronic Resource
    Electronic Resource
    Springer
    Journal of applied mechanics and technical physics 34 (1993), S. 219-226 
    ISSN: 1573-8620
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Type of Medium: Electronic Resource
    Library Location Call Number Volume/Issue/Year Availability
    BibTip Others were also interested in ...
  • 6
    Electronic Resource
    Electronic Resource
    Springer
    Journal of mathematical sciences 49 (1990), S. 715-799 
    ISSN: 1573-8795
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mathematics
    Notes: Abstract In the first part of the paper there is given a survey of the contemporary state of the theory of the sufficient univalence and p-valence conditions for analytic and meromorphic functions of a complex variable. The second part is devoted to a survey of the results on the conditions for the univalent solvability of applied inverse boundary value problems.
    Type of Medium: Electronic Resource
    Library Location Call Number Volume/Issue/Year Availability
    BibTip Others were also interested in ...
  • 7
    Electronic Resource
    Electronic Resource
    Chichester [u.a.] : Wiley-Blackwell
    International Journal for Numerical Methods in Engineering 35 (1992), S. 121-132 
    ISSN: 0029-5981
    Keywords: Engineering ; Engineering General
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Mathematics , Technology
    Notes: A simple and reliable method of aerodynamic design of airfoils is proposed for a given range of the angle of attack. The method is based on the solution of a new inverse boundary-value problem of aerohydrodynamics. In the problem the initial velocity distributions are given along the contour of the required airfoil as a function of the are co-ordinate for extreme values of the angle of attack from a fixed range. We justify a method of choice of these distributions which guarantees a non-stalling flow around the airfoil. The problem of airfoil optimization is also considered. Results of numerical calculations are presented.
    Additional Material: 10 Ill.
    Type of Medium: Electronic Resource
    Library Location Call Number Volume/Issue/Year Availability
    BibTip Others were also interested in ...
Close ⊗
This website uses cookies and the analysis tool Matomo. More information can be found here...