We read every piece of feedback, and take your input very seriously.
To see all available qualifiers, see our documentation.
Have a question about this project? Sign up for a free GitHub account to open an issue and contact its maintainers and the community.
By clicking “Sign up for GitHub”, you agree to our terms of service and privacy statement. We’ll occasionally send you account related emails.
Already on GitHub? Sign in to your account
High pressure and low pressure turbines (n2 and n1 accordingly) has a bit higher RPM percentage then they should.
Reference table from PT flight manual:
For example, on takeoff thrust n2 and n1 are 96.5% and 101% instead of 95.5% and 97%.
The text was updated successfully, but these errors were encountered:
ShFsn
No branches or pull requests
High pressure and low pressure turbines (n2 and n1 accordingly) has a bit higher RPM percentage then they should.
Reference table from PT flight manual:
For example, on takeoff thrust n2 and n1 are 96.5% and 101% instead of 95.5% and 97%.
The text was updated successfully, but these errors were encountered: