Method of evaluating analytically matching problems of engine design vs airplane design uses presentation of airplane performance which facilitates determination of range or endurance as function of primary engine performance and engine weight requirements of airplane; method is illustrated by matching series of theoretically defined regenerative and nonregenerative turbofan engines with varying bypass ratios to laminar and turbulent aircraft of typical cruise speed; all of engines are front fan configurations with fans geared to gas generators at bypass ratios greater than 4.0.


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    Title :

    Method of determining propulsion system requirements for long-range, long-endurance aircraft


    Additional title:

    J Aircraft


    Contributors:

    Published in:

    Publication date :

    1965


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






    Requirements for long range -- Long endurance aircraft

    Wheaton, R.J. / Bogdanovic, J.A. / Feder, A. | Engineering Index Backfile | 1964


    REQUIREMENTS FOR LONG RANGE -LONG ENDURANCE AIRCRAFT

    Feder, A. / Bogdanovic, J.A. / Wheaton, R.J. | SAE Technical Papers | 1964


    Propulsion System Technologies for Long Range and Long Endurance Aircraft

    Garwood, K. R. / North Atlantic Treaty Organization | British Library Conference Proceedings | 1993