Ch-46 Composite Rotor Blade Flight Stress Survey Data, Volume XII. Tabulated Forward and Aft Rotor Shaft Loads, Load Factor, Pitch and Roll Attitude and Rotor RPM

Ch-46 Composite Rotor Blade Flight Stress Survey Data, Volume XII. Tabulated Forward and Aft Rotor Shaft Loads, Load Factor, Pitch and Roll Attitude and Rotor RPM

This volume contains measured steady and alternating forward and aft rotor shaft loads tabulated by flight and event number. Maximum and minimum forward and aft shaft torque values are included in this grouping. The steady and alternating data is plotted versus true airspeed and can be found in Volu...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Aiello ,R, Bendo,J
Format: Report
Sprache:eng
Schlagworte:
AERODYNAMIC LOADING
AIRSPEED
BENDING STRESS
CH-46E aircraft
COMPOSITE MATERIALS
DATA BASES
DRIVE SHAFTS
FLIGHT LOADS
FLIGHT MANEUVERS
FLIGHT TESTING
H-46 aircraft
HELICOPTER ROTORS
Helicopters
Mechanics
PITCH(MOTION)
ROLL
ROTOR BLADES(ROTARY WINGS)
STRESSES
TABLES(DATA)
TORQUE
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:This volume contains measured steady and alternating forward and aft rotor shaft loads tabulated by flight and event number. Maximum and minimum forward and aft shaft torque values are included in this grouping. The steady and alternating data is plotted versus true airspeed and can be found in Volume 8. In addition, this volume contains measured (steady, maximum and minimum) load factor, pitch/roll attitude, and rotor rpm tabulated by flight and event number. See also Volume 1, AD-A075 566.