MARTIN HOLLMANN – B.S., California State University at San Jose
Submitted in partial fulfillment of the requirements for the degree of Master of Science in Engineering in the Graduate Studies Program of Florida Technological University.
Orlando, Florida 1974
ACKNOWLEDGMENTS
The author wishes to express his gratitude to I.D. Keiter from the McCauley Corporation for making available the Hamilton Standard Method of Propeller Performance Calculation and R. J. Moore of Teledyne Continental Motors for sending the engine specifications used in CAGR0S.
I am especially thankful to Dr. Henry A. Hagedoorn, my thesis advisor, for his encouragement, patience, and assistance during the preparation of this thesis.
104 Pages of study materials
Martin Hollmann
Dec. 1940 to Oct. 2012
Life legacy
President of Aircraft Designs, Inc.
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Hollmann Gyrocopter
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