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Analysis of an Optimal Flight Path of Subsonic Transport Aircraft for Fuel Saving
-
Y. Tsujikawa,
Published/Copyright:
September 1, 1995
Published Online: 1995-09
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- A Navier-Stokes Analysis of a Controlled-Diffusion Compressor Cascade at Increasing Inlet Flow Angles
- Extinction Dynamics of Partially Premised Spray Flames
- Analysis of an Optimal Flight Path of Subsonic Transport Aircraft for Fuel Saving
- The Potential of Gas Turbine Propulsion in Modern Merchant Shipping
- A Unified Variable-Domain Variational Theory of Hybrid Problems for Compressible S2-Flow in Mixed-Flow Turbomachinery
- Effect of Tip Clearance at Midspan Section of Controlled Diffusion Compressor Cascade
- Optimization of Axial-Flow Pump Cascade Solidity Subject to Cavitation- and Separation-Free Constraints
Articles in the same Issue
- CONTENTS
- A Navier-Stokes Analysis of a Controlled-Diffusion Compressor Cascade at Increasing Inlet Flow Angles
- Extinction Dynamics of Partially Premised Spray Flames
- Analysis of an Optimal Flight Path of Subsonic Transport Aircraft for Fuel Saving
- The Potential of Gas Turbine Propulsion in Modern Merchant Shipping
- A Unified Variable-Domain Variational Theory of Hybrid Problems for Compressible S2-Flow in Mixed-Flow Turbomachinery
- Effect of Tip Clearance at Midspan Section of Controlled Diffusion Compressor Cascade
- Optimization of Axial-Flow Pump Cascade Solidity Subject to Cavitation- and Separation-Free Constraints
