1-24 of 27 Books
Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover
Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover
By Ian G. Fejtek
XV-15 structural-acoustic data
XV-15 structural-acoustic data
By Karen H. Lyle
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
By Donald R. Riley
Analysis of small-scale rotor hover performance data
Analysis of small-scale rotor hover performance data
By Cahit Kitaplioglu
Aeroelastic stability of a full-scale hingeless rotor
Aeroelastic stability of a full-scale hingeless rotor
By Randall L. Peterson
3-D wake measurements near a hovering rotor for determining profile and induced drag
3-D wake measurements near a hovering rotor for determining profile and induced drag
By Kenneth W. McAlister
Free wake analysis of hover performance using a new influence coefficient method
Free wake analysis of hover performance using a new influence coefficient method
By Todd R. Quackenbush
Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft
Stereopsis cueing effects on hover-in-turbulence performance in a simulated rotorcraft
By Russell V. Parrish
Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor
Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor
By Arthur E. Phelps
Description of the U.S. Army small-scale 2-meter rotor test system
Description of the U.S. Army small-scale 2-meter rotor test system
By Arthur E. Phelps
Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft
Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft
By James A. Franklin
The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
By William G. Bousman
Design and evaluation of a cockpit display for hovering flight
Design and evaluation of a cockpit display for hovering flight
By Ronald A. Hess
Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades
Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades
By J. D. Baeder
Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover
Documentation of ice shapes on the main rotor of a UH-1H helicopter in hover
By John D. Lee
Solution method for a hovering helicopter rotor using the Euler equations
Solution method for a hovering helicopter rotor using the Euler equations
By Thomas W. Roberts
Navier-Stokes calculations of the flowfield of a helicopter rotor in hover
Navier-Stokes calculations of the flowfield of a helicopter rotor in hover
By R. K. Agarwal
Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover
Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover
By James A. Franklin
Preliminary investigation of motion requirements for the simulation of helicopter hover tasks
Preliminary investigation of motion requirements for the simulation of helicopter hover tasks
By Russell V. Parrish
Experimental and analytical studies of a model helicopter rotor in hover
Experimental and analytical studies of a model helicopter rotor in hover
By Francis X. Caradonna
Flow field around a hovering rotor
Flow field around a hovering rotor
By C. Tung
Performance and pressure data from a small model tilt-rotor in hover
Performance and pressure data from a small model tilt-rotor in hover
By Lonnie Branum
A two dimensional study of rotor/airfoil interaction in hover
A two dimensional study of rotor/airfoil interaction in hover
By Chyang Sheng Lee
Wide speed range turboshaft study
Wide speed range turboshaft study
By Martin D'Angelo