The phrase "analysis of aerospace" is correct and usable in written English.
It can be used in contexts related to the study or examination of aerospace technology, engineering, or industry trends.
Example: "The analysis of aerospace innovations reveals significant advancements in fuel efficiency and safety."
Alternatives: "study of aerospace" or "examination of aerospace".
The paper describes the analysis of aerospace composite structures under dynamic loading.
It can provide some guidance for the design and performance analysis of aerospace embedded computers.
This chapter reviews the most recent developments in the field of analytical techniques used in failure analysis of aerospace, chemical, and oil and gas industries.
Therefore, the developed model can be applied to engineering calculation, e.g. pre-stretching analysis of aerospace aluminium thick plate, with acceptable accuracy.
This chapter focuses on the second major distinction in the exergy analysis of aerospace as opposed to ground-based systems: the variation in the operating environment.
We have implemented these ideas in a CORBA/Java framework for distributed computing, and are currently applying them to a distributed system for the analysis of aerospace design (wind-tunnel and CFD) data.
Significantly, this paper details a structural reliability analysis of a complex aerospace structure for which little statistical information is available.
Detailed aerothermal analysis of a high speed aerospace vehicle with multiple lateral jets is carried out in its full trajectory covering wide range of Mach numbers and altitudes.
This study addresses that gap through an analysis of 3488 citations from aerospace engineering faculty publications by source, format, age, and subject.
This is followed by a full case study analysis of how a leading aerospace company, Short Brothers (now known as Bombardier Aerospace Shorts), have transformed themselves since privatisation from an organisation in crisis to a leading performer in their market sector.
The method is applicable to delamination propagation within the Paris-law regime and is suitable for the analysis of three-dimensional structures typical of aerospace applications.
