Landing Approach Airframe Noise Measurements and Analysis
Highly Integrated Digital Engine Control System on an F-15 Airplane
Predicted Performance Benefits of an Adaptive Digital Engine Control System of an F-15 Airplane
Summary of Results of NASA F-15 Flight Research Program
Value of Early Flight Evaluation of Propulsion Concepts Using the NASA F-15 Research Airplane
Integrated Flight-Propulsion Control Concepts for Supersonic Transport Airplanes
Controlling Crippled Aircraft-with Throttles
Preliminary Investigation of the Use of Throttles for Emergency Flight Control
Flight Testing and Simulation of an F-15 Airplane Using Throttles for Flight Control
Flight-Determined Benefits of Integrated Flight-Propulsion Control Systems
Preliminary Flight Results of a Fly-by-Throttle Emergency Flight Control System on an F-15 Airplane
Flight Testing a Propulsion-Controlled Aircraft Emergency Flight Control System on an F-15 Airplane
Flight Research Using F100 Engine P680063 in the NASA F-15 Airplane
Background and Principles of Throttles-Only Flight Control
Overview of Integrated Flight-Propulsion Controls Flight Research on the NASA F-15 Research Airplane
Flight Test of a Propulsion Controlled Aircraft System on the NASA F-15 Airplane