Method used by H. TSIEN to derive similarity rules for hypersonic flows is utilized to derive T. von KARMAN's similarity rules for transonic flows; at lower limit of transonic region of flow theory yields formula for critical stream Mach numbers of given family of symmetrical profiles; this formula can also be obtained by means of Prandtl-Glauert smallperturbation theory.
On similarity rules for transonic flows
Nat Advisory Committee Aeronautics -- Tech Note
1948
16 pages
Report
English
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On Similarity Rules for Transonic Flows
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|On similarity rules for transonic flows
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|On similarity rules for transonic flows
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|On similarity rules for transonic flows
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