Matching engine and aircraft lapse rates for high speed civil aircraft
- Author
- SALAY, C. R1 ; ELLIOTT, D. W1
[1] General Electric Aircraft Engines, Cincinnati, Ohio 45215, United States - Conference name
- AIAA/SAE/ASME/ASEE. Joint Propulsion Conference and Exhibit (29 ; Monterey, CA 1993-06-28)
- Source
Journal of aircraft. 1996, Vol 33, Num 1, pp 61-67 ; ref : 1 ref
- CODEN
- JAIRAM
- ISSN
- 0021-8669
- Scientific domain
- Aeronautics astronautics; Mechanical engineering; Mechanics acoustics; Transportation
- Publisher
- American Institute of Aeronautics and Astronautics, Reston, VA
- Publication country
- United States
- Document type
- Conference Paper
- Language
- English
- Keyword (fr)
- Aéronef Cycle Défaillance Moteur Optimisation Poussée Système propulsion Turboréacteur double flux Adaptation
- Keyword (en)
- Aircraft Cycle Failures Engine Optimization Thrust Propulsion systems Turbofan engine Matching
- Keyword (es)
- Aeronave Ciclo Fallo Motor Optimización Empujón Turboreactor doble flujo
- Classification
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D15 Ground, air and sea transportation, marine construction / 001D15J Miscellaneous transportation
- Discipline
- Building. Public works. Transport. Civil engineering
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 3106147
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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DOI
10.2514/3.46903 
https://dx.doi.org/10.2514/3.46903
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