This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Turbine Engine Technology and Cost
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1970 by SAE International in United States
Annotation ability available
An analysis was conducted on a total of 106,000 turbojet and turbofan engines procured by the United States Air Force to ascertain if an aircraft turbine engine's cost can be effectively correlated to its technical performance. Results indicate that such technical parameters are not valid and other factors such as military situation, economic conditions, and procurement situation should be investigated.
|Technical Paper||Navy Development of Low-Cost Supersonic Turbojet Engines|
|Technical Paper||Design Consideration for a Generic E.V.M.|
|Technical Paper||Low-Weight, Low Cost AC/DC Converter for the V-22|
CitationSeely, G. and Stibich, M., "Turbine Engine Technology and Cost," SAE Technical Paper 700270, 1970, https://doi.org/10.4271/700270.
- “USAF Propulsion Characteristics Summary (Airbreathing).” Aeronautical Systems Division Gray Book I December 1967