Constant Altitude-Constant Mach Number Cruise Range of Transport Aircraft with Compressibility Effects
Author:
Affiliation:
1. Anadolu University, 26470 Eskisehir, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.14252
Reference20 articles.
1. Optimum cruise lift coefficient in initial design of jet aircraft
2. Comparison of Generalized Approximate Cruise Range Solutions for Turbojet/Fan Aircraft
3. Approximate solutions of range for constant altitude – constant high subsonic speed flight of transport aircraft
4. Cruise performance and range prediction reconsidered
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