The Bombardier CSeries and the Boeing 737 are two aircraft in the same class. Their nose shapes are very different from each other though as can be seen in these two images. What are the major aerodynamic differences between these two nose designs?
CSeries:
Image Source
Boeing 737:
Image Source
Note: This question and answer set don't really answer my question here because it talks about a generic nose form of aircraft made by Boeing and Airbus. I am looking for specific aerodynamic differences between nose cone shapes on specific models of Boeing and Bombardier aircraft. The Airbus part of that question cannot answer the Bombardier part of this question.
That question also does not talk about specific model as it says at the bottom:
This image is only an example and my question is not about any specific model.
I want the specifics for the nose cone shapes of Boeing 737 and the Bombardier CSeries, not specifics on the aircraft themselves. This is more like asking for for the aerodynamic difference, for example, between a blunt nose and an ogive nose than something to do with aircraft corporations.