Could an NMA be made good enough? Part 5

By Bjorn Fehrm

Subscription Required

Introduction

April 20, 2017, © Leeham Co.: After defining the fuselage and wings, it’s now time for the engines.  We go through the sizing criteria for engines for airliners and find the size of engine that is needed for the NMA.

The NMA will need engines which are larger than the single aisle engines for Airbus’ A320neo and Boeing’s 737 MAX. But they will be smaller than the next size up for modern engines, the GEnx-2B for Boeing’s 747-8.

Figure 1. The NMA takes more and more the shape of a 767 replacement (A United 767-200). Source: United

This means the NMA will need new engines, at least 50% larger than the present engines designed for A320neo and 737 MAX.

Summary:

  • An NMA engine will be sized by V2 safety speed or Maximum Continuous Thrust (MCT) criteria.
  • The normal Top of Climb (ToC) sizing point will be less stressing for a twin engine airliner like NMA.

To read the rest of the article Login or Subscribe today.