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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
61

A vortex wake analysis of optimum high by-pass ratio ducted fans

Janakiram, Damaraju Subramanya 12 1900 (has links)
No description available.
62

Coupled elastic rotor/body vibrations with inplane degrees of freedom

Huang, Ming-Sheng 05 1900 (has links)
No description available.
63

Study of an asymptotic method for helicopter rotor blade aerodynamic loads

Vaidyanathan, Anand Ramabhadran 12 1900 (has links)
No description available.
64

An examination of the effect of the variable part of blade circulation on the induced power requirements of a two-bladed rotor in forward flight by an electromagnetic analog

Corley, William Lawrence 12 1900 (has links)
No description available.
65

The normal component of induced velocity for a lifting rotor in ground effect

Tow, James Lyons 05 1900 (has links)
No description available.
66

On the indentification of harmonic loads and inflow of a coupled bending-torsion helicopter rotor blade

Higman, Jerry Paul 05 1900 (has links)
No description available.
67

Aeroelastic stability of composite hingeless rotors with finite-state unsteady aerodynamics

Shang, Xiaoyang 08 1900 (has links)
No description available.
68

A derivation of rotor blade equations of motion in forward flight and their solution

Jonnalagadda, V. R. Prasad 08 1900 (has links)
No description available.
69

The correction of current lifting rotor theory for the effects of the radial velocity component

Cunningham, Charles Richard 05 1900 (has links)
No description available.
70

Velocity measurements near the blade tip and in the tip vortex core of a hovering model rotor

Thompson, Thomas L. 12 1900 (has links)
No description available.

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