Analysis of Response Requirements for V/STOL Lift/Cruise Engines Used to Provide Height and Moment Control.

摘要

Parametric investigations were performed to determine constrainst imposed by handling qualities requirements on a V/STOL lift/cruise propulsion system when used to provide at least a portion of the vehicle moment control. Primary emphasis was placed on defining the magnitude of engine response time and incremental thrust necessary to satisfy the applicable requirements of the V/STOL Flying Qualities Specification, MIL-F-83300. Where possible the results were normalized by baseline aircraft parameters to eliminate configuration dependence.