Skip to main content
SpringerLink
Log in

On the flow of an unsteady compressible boundary layer over a semi-infinite flat plate whose temperature exceeds the free stream temperature

  • Brief Reports
  • Published:
Zeitschrift für angewandte Mathematik und Physik ZAMP Aims and scope Submit manuscript

Zusammenfassung

Es wird die Grenzschicht untersucht, die sich in laminarer, kompressibler Strömung an einer ebenen Platte einstellt, die sich nach einer Seite ins Unendliche ausdehnt und von der Ruhe aus gleichförmig beschleunigt bewegt wird. Die Veränderlichkeit des Produktes aus Dichte und Zähigkeit innerhalb der Grenzschicht wird berücksichtigt. Der Effekt dieser Veränderlichkeit kurz nach Beginn der Bewegung wird für Punkte berechnet, die weit vom Plattenrand entfernt sind.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

References

  1. F. K. Moore,Unsteady Laminar Boundary Layer Flow, NACA Technical Note 2471, September 1951.

  2. S. Ostrach,Compressible Laminar Boundary Layer and Heat Transfer for Unsteady Motions of a Flat Plate, NACA Technical Note 3569, November 1955.

  3. F. K. Moore andS. Ostrach,Average Properties of Compressible Laminar Boundary Layer on Flat Plate With Unsteady Flight Velocity, NACA Technical Note 3886, December 1956.

  4. N. A. Evans,Heat Transfer in the Unsteady Compressible Laminar Boundary Layer on a Flat Plate, Proceedings of the 1960 Heat Transfer and Fluid Mechanics Institute, Stanford University, Stanford, California, pp. 77–87.

  5. N. B. Cohen,Correlation Formulas and Tables of Density and Some Transport Properties of Equilibrium Dissociating Air for Use in the Solutions of the Boundary Layer Equations, NASA Technical Note D-194, February 1960.

Download references

Author information

Authors and Affiliations

  1. Department of Aerospace Engineering, University of Maryland, College Park, Maryland, USA

    Stefan Schreier

Authors
  1. Stefan Schreier
    View author publications

    You can also search for this author in PubMed Google Scholar

Additional information

Subscriptsx, t and η indicate differentiation

The computer time for this project was supported by National Aeronautics and Space Administration Grant NsG-398 to the Computer Science Center of the University of Maryland.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Schreier, S. On the flow of an unsteady compressible boundary layer over a semi-infinite flat plate whose temperature exceeds the free stream temperature. Journal of Applied Mathematics and Physics (ZAMP) 17, 541–544 (1966). https://doi.org/10.1007/BF01595989

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF01595989

Keywords

Search

Navigation