HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM “WEIGHT AND BALANCE STUDIES” VOLUME VII

摘要

Volume VII of Heavy-Lift Tip Turbojet Rotor System discusses statistical, analytical, and empirical weight analysis methods used to evaluate the empty weight of the helicopter. Blade lag characteristics are also discussed, including an analysis showing blade lag angles with one and two engines inoperative. Included are aircraft balance predictions.