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This report describes an effort undertaken to improve small gas turbine combustor design I techniques. This analytical procedure is viewed as a significant step toward reducing the design and development time and the cost associated with future Army gas turbine combustors while simultaneously achieving a more durable and fuel-efficient design. The reader is referred to the report documentation page for a description of each of the three volumes of this report. It Is considered worthy of widespread application with the turbine Industry. Any critique or other response regarding its use should be addressed to this agency. Mr. Kent Smith of the Propulsion Technical Area, Aeronautical Technology Division, served as Project Engineer for this effort. '3 DISCLAIMERS The findings In this report are not to be construed as en official Department of the Army position unless so designated by other authorized documents. Mhen Government drawings, specifications, or other date are used for any purpose other then In connection with a definitely related Government procuremnent operation, the United $tate Government thereby Incurs no responsibility nor eny obligation whatsoever; and the fact that the Government may have formulated, furnished, or in any way supplied the sald drawings. specifications, or other date is not to be regarded by Implication or otherwise as in any manner licensing the holder or any other person or corporation, or conveylng any rights or permission, to rmanufacture, use, or sell any patented invention that may in any way be related thereto. Trade names cited in this report do not constitute en officiil endorsement or approval of the use of such h commercial hardware or softwsre, ,,POel 1" ION TRUCTIONS Destroy this report whon no longer needeld, D0 not return it to the originito,. Unclassi~fied SECWRIT'I CLASSIFICATION OF THIS PAO&E (fton, Data Sniet.d)

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