Optimum cruise lift coefficient in initial design of jet aircraft
- 1 July 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 29 (4) , 712-714
- https://doi.org/10.2514/3.46226
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Preliminary design of civil transport aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Toward an unsteady-flow airplanePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Reducing fuel consumption of subsonic aircraft by optimal cyclic cruiseJournal of Aircraft, 1987
- Dynamic stall inception correlation for airfoils undergoing constantpitch rate motionsAIAA Journal, 1986
- Generalized maximum specific range performanceJournal of Aircraft, 1983
- Estimation of aircraft fuel consumptionJournal of Aircraft, 1982
- Prediction of range and endurance of jet aircraft at constant altitudeJournal of Aircraft, 1981
- Multivariate optimum design of subsonic jet passenger airplaneJournal of Aircraft, 1980
- The general arrangementPublished by Springer Nature ,1976