Research of a wind tunnel parameters by means of cross-section analysis of air flow profiles-Reference-Cited by-同舟云学术

Research of a wind tunnel parameters by means of cross-section analysis of air flow profiles

Published:2019 Issue: Volume: Page:
ISSN:0094-243X
Container-title:18TH CONFERENCE OF POWER SYSTEM ENGINEERING, THERMODYNAMICS AND FLUID MECHANICS
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Author:

Yanovych Vitalii,Duda Daniel,Horáček Vít,Uruba Václav

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5138636

Reference12 articles.

1. L. Prandtl, Ubr “Flussigkeitsbewegung bei sehr Kleiner Reibung”, Verh. d. 3 Int. Math.-Kongr., Heilderberg, Leipzig: Teubner, 484–491 (1905).

2. On the solution of the laminar boundary layer equations.

3. ON LAMINAR BOUNDARY-LAYER FLOW NEAR A POSITION OF SEPARATION

4. J. Ackeret, F. Feldman and N. Rott, “Investigation of compression shocks and boundary layers in gases moving at high speed”. NACA Tech. Note 1113, 1947.

5. The Interaction Between Boundary Layer and Shock Waves in Transonic Flow

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