Aerodynamics

• NASA TN D-3845 Rolling stability derivatives of a variable-sweep tactical fighter model at subsonic speeds
  William P. Henderson/ W. Pelham Phillips and Thomas G.Gainer
  February 1967
• NASA TN D-6490 Comparison of in-flight F-111A inlet performance for on and off-scheduled inlet geometry at mach numbers of 0.68 to 2.18
  Richard A. Martin and Donald L. Hughes

These are the data sources for the F-14B Simulator for Flightgear

These are the data sources / references for my FlightGear F-15. The FDM is based on the windtunnel derived aerodynamic data found in (AFIT/GAE/ENY/90D-16).