Title: BOUNDARY LAYER STABILIZATION BY DISTRIBUTED DAMPING
Abstract: Naval Engineers JournalVolume 74, Issue 2 p. 341-348 BOUNDARY LAYER STABILIZATION BY DISTRIBUTED DAMPING Dr. MAX O. KRAMER, Dr. MAX O. KRAMER THE AUTHOR was born in Koeln, Germany, on September 8, 1903. He graduated in Electronics at the University of Munich, Germany in 1926 and received the Doctor of Science Diploma at the University of Aachen, Germany, in 1931 while working at the Aerodynamic Institute under Professor Theodore Von Karman. From 1932 to 1943, he was employed by the German Research Center for Aeronautics (DVL, Berlin, Germany) where he ultimately headed the Aerodynamic Institute and was appointed Senator, or member of the leading staff. From 1943 to 1945, he headed the Development Station for Guided Missiles at Brackwede, Germany, which developed the remote controlled fighter-borne Rocket X-4. From 1947 to 1952, he worked at the Naval Air Development Center, Johnsville, Pa., where he developed an acoustic guidance system for guided missiles. In 1952 he was employed by Coleman Engineering Company, Inc., Los Angeles, California, as Technical Director supervising various research projects. When in 1956, it was decided to concentrate on an invention of his called "Boundary Layer Stabilization by Distributed Damping," a subsidiary company, Coleman-Kramer Inc., Los Angeles, was formed for the purpose. He was Vice President of this company. At the end of 1960, the activity of Coleman-Kramer Inc. as well as that of its parent company, Coleman Engineering Company, Inc., had to be terminated for financial reasons. At that time, he bought the research equipment of Coleman-Kramer Inc. and continued his research on his own.Search for more papers by this author Dr. MAX O. KRAMER, Dr. MAX O. KRAMER THE AUTHOR was born in Koeln, Germany, on September 8, 1903. He graduated in Electronics at the University of Munich, Germany in 1926 and received the Doctor of Science Diploma at the University of Aachen, Germany, in 1931 while working at the Aerodynamic Institute under Professor Theodore Von Karman. From 1932 to 1943, he was employed by the German Research Center for Aeronautics (DVL, Berlin, Germany) where he ultimately headed the Aerodynamic Institute and was appointed Senator, or member of the leading staff. From 1943 to 1945, he headed the Development Station for Guided Missiles at Brackwede, Germany, which developed the remote controlled fighter-borne Rocket X-4. From 1947 to 1952, he worked at the Naval Air Development Center, Johnsville, Pa., where he developed an acoustic guidance system for guided missiles. In 1952 he was employed by Coleman Engineering Company, Inc., Los Angeles, California, as Technical Director supervising various research projects. When in 1956, it was decided to concentrate on an invention of his called "Boundary Layer Stabilization by Distributed Damping," a subsidiary company, Coleman-Kramer Inc., Los Angeles, was formed for the purpose. He was Vice President of this company. At the end of 1960, the activity of Coleman-Kramer Inc. as well as that of its parent company, Coleman Engineering Company, Inc., had to be terminated for financial reasons. At that time, he bought the research equipment of Coleman-Kramer Inc. and continued his research on his own.Search for more papers by this author First published: May 1962 https://doi.org/10.1111/j.1559-3584.1962.tb05568.xCitations: 74 AboutPDF ToolsExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onEmailFacebookTwitterLinkedInRedditWechat REFERENCES 1 Kramer, Max O., "Boundary Layer Stabilization by Distributed Damping," Journal of the Aeronautical Sciences, Vol. 24, No. 6, June, 1957. Web of Science®Google Scholar 2 Kramer, Max O., "Boundary Layer Stabilization by Distributed Damping," Journal Of The American Society Of Naval Engineers, Inc., February, 1960, pp. 25–33. PubMedGoogle Scholar 3 Schubauer, G. B. and Skramstad, H. K., "Laminar Boundary Oscillations and Stability of Laminar Flow," Journal of the Aeronautical Sciences, Vol. 14, No. 2, pp. 71, February, 1947. 10.2514/8.1267 Google Scholar Citing Literature Volume74, Issue2May 1962Pages 341-348 ReferencesRelatedInformation
Publication Year: 1962
Publication Date: 1962-05-01
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 195
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