Summary of studies of helicopter rotor icing.

"Contract No. AF 33(616)-2859."

A method for predicting the aerodynamic loads and dynamic response of the rotor blades of a tandem-rotor helicopter.

"USAAVLABS technical report 67-38."

Computed moisture interception on helicopter rotor blades,

"Contract no. AF 33(616)-2859."

Horizontal-axis wind system rotor performance model comparison : a compendium /

"February 1983."

Investigation of helicopter rotor blade flutter and flapwise bending response in hovering

"Propulsion Laboratory, Contract no. AF33(616)-5210, Project no. 3137, Task no. 33113."

Boundary layer and wake modifications to compressor design systems : the effect of blade-to-blade flow variations on the mean flow field of a transonic rotor : final report, 01 September 1976-31 August 1978 /

"AFAPL-TR-79-2010."

Aerodynamic characteristics of helicopter rotors; rotor contributions to helicopter stability parameters

Mode of access: Internet.

Computed induced velocity, induced drag, and angle of attack distributions for a two-bladed rotor

Cover title.