An analysis of maximum range cruise including wind effects
Authors:
- Damián RivasDRDamián Rivas
- Oscar Lopez-GarciaOLOscar Lopez-Garcia
- Sergio EstebanSergio Esteban
- Eduardo GalloEduardo Gallo
- 28 February 2010
- journal article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 14 (1) , 38-48
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Compressibility Effects on Maximum Range Cruise at Constant AltitudeJournal of Guidance, Control, and Dynamics, 2009
- Simplified Thrust and Fuel Consumption Models for Modern Two-Shaft Turbofan EnginesJournal of Aircraft, 2008
- Constant Altitude-Constant Mach Number Cruise Range of Transport Aircraft with Compressibility EffectsJournal of Aircraft, 2006
- Approximate solutions of range for constant altitude – constant high subsonic speed flight of transport aircraftAerospace Science and Technology, 2004
- An Introduction to Aircraft Performance1997
- Optimal cruise performanceJournal of Aircraft, 1993
- Optimum cruise lift coefficient in initial design of jet aircraftJournal of Aircraft, 1992
- Reducing fuel consumption of subsonic aircraft by optimal cyclic cruiseJournal of Aircraft, 1987
- Errata: Effects of Wind on Aircraft Cruise PerformanceJournal of Aircraft, 1981
- Effects of Wind on Aircraft Cruise PerformanceJournal of Aircraft, 1979