Theoretical Pressure Distributions on Wings of Finite Span at Zero Incidence for Mach Numbers Near 1
Author: Alberta Y. Alksne
Publisher:
Published: 1961
Total Pages: 56
ISBN-13:
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Author: Alberta Y. Alksne
Publisher:
Published: 1961
Total Pages: 56
ISBN-13:
DOWNLOAD EBOOKAuthor: Alberta Y. Alksne
Publisher:
Published: 1961
Total Pages: 0
ISBN-13:
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Publisher:
Published:
Total Pages: 1284
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Publisher:
Published: 1967
Total Pages: 1352
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DOWNLOAD EBOOKAuthor: K. Oswatitsch
Publisher: Springer Science & Business Media
Published: 2012-12-06
Total Pages: 591
ISBN-13: 3642810055
DOWNLOAD EBOOKThe first Symposium Transsonicum took pl.ace in Aachen thirteen years ago during a period of decreasing governmental. and industrial. support for transonic flow research. Since then, there has been a strong revival. in interest in transonic flow research so that the number of partici pants at the second symposium remained about the same as at the first even in spite of tight financial. means and Limited governmental. support. During both meetings the number of participants reached the upper Limit of the number desirabl.e for such a symposium. Participants came from aU over the worl.d and there was a weU bal.anced distribution of participants from aU countries interested in transonic flow research. The discussions - mostLy conducted in EngLish - were stimul.ating and there was a great deal. of interest in the l.ectures as was shown by the good attendance even during the l.ast session on Saturday morning.
Author: United States. Superintendent of Documents
Publisher:
Published: 1980
Total Pages: 1284
ISBN-13:
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Publisher:
Published: 1973
Total Pages: 568
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DOWNLOAD EBOOKAuthor: John R. Spreiter
Publisher:
Published: 1971
Total Pages: 936
ISBN-13:
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Publisher:
Published: 1981
Total Pages: 710
ISBN-13:
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