Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine
Title
Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine / Carlos L. Blacklock, project Manager; Dr. Jan Roskam, principal Investigator.
Published by
Lawrence, Kansas : Flight Research Laboratory, University of Kansas Center for Research, Inc. ; [Hampton, Virginia] : National Aeronautics and Space Administration, Langley Research Center, October 1983.
3 microfiches (vi, 193 unnumbered pages) : negative, illustrations; 11 x 15 cm.
Summary
"The results of static performance tests were carried out on an ultralight engine. A Cuyuna 430 cc, 2 stroke, 2 cylinder model was used to measure thrust, torque, propeller RPM, fuel flow, cylinder head temperature, and change in pressure through the propeller. Measurement of each of the above parameters was taken at specific values of RPM. The propeller's RPM's ranged from idle at approximately 750 RPM to a maximum value of 2810 RPM. The test results were then manipulated to obtain thrust coefficient, power coefficient, shaft horse power, and shaft specific fuel consumption."--NTIS abstract.
"Prepared under NASA Grant NAG1-345 for National Aeronautics and Space Administration, Langley Research Center."
Bibliography (note)
Includes bibliographical references (page 6.1).
Funding (note)
Sponsored by the National Aeronautics and Space Administration, Langley Research Center
Author
Roskam, Jan, 1930- author.
Title
Determination of the static performance of a Cuyuna 430 cc. model UL-430RR engine / Carlos L. Blacklock, project Manager; Dr. Jan Roskam, principal Investigator.
Publisher
Lawrence, Kansas : Flight Research Laboratory, University of Kansas Center for Research, Inc. ; [Hampton, Virginia] : National Aeronautics and Space Administration, Langley Research Center, October 1983.
Type of content
text
Type of medium
microform
Type of carrier
microfiche
Series
NASA-CR ; 175354
NASA contractor report ; NASA CR-175354.
Bibliography
Includes bibliographical references (page 6.1).
Funding
Sponsored by the National Aeronautics and Space Administration, Langley Research Center NAG1-345 KU-FRL-6135-1