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Inclusion of Tip Relief in the Prediction of Compressibility Effects on Helicopter Rotor Performance
Abstract : The tip relief effect on the performance of helicopters operating at high subsonic tip Mach numbers is calculated. The theoretical method based on the complementary wing model for tipExpand
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Review and Preliminary Evaluation of Lifting Horizontal-Axis Rotating-Wing Aeronautical Systems (HARWAS)
Abstract : Among the purely aeronautical applications, near-horizontal axis as well as horizontal axis devices are considered. The former cover the radial-lift propeller or 'self-propelling' wing;Expand
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Aerodynamic Theory of the Annular Jet
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INVESTIGATION OF LIGHTWEIGHT STRUCTURAL DESIGN TECHNIQUES FOR LIGHTWEIGHT FANS
Abstract : The results of an investigation of the design and fabrication problems of a minimum-weight rotating-diffuser lift system for an air cushion vehicle (ACV) are presented. A numerical methodExpand
AERODYNAMIC TESTING OF AN AIRBORNE LIGHTWEIGHT HIGH-EFFICIENCY RADIAL FAN.
Abstract : The results of the aerodynamic testing of a 66-inch diameter rotating-diffuser centrifugal fan for internal flow airborne applications are presented. To accommodate the testing of thisExpand
AERODYNAMIC THEORY OF THE ANNULAR JET. PART I
A SOLUTION OF THE TWO-DIMENSIONAL TURBULENT VISCOUS CURVED JET USING THE IBM 7090 COMPUTER
Abstract : A numerical solution of the two-dimensional curved turbulent and incompressible jet flow, using the IBM 7090 computer, is presented. This solution is a straight-forward extension of theExpand
Plan to achieve national energy independence
Mr. Fung's plan is intended to buy us time to get to practical renewable-energy sources and consists of four broad approaches: active and passive energy-conservation measures, alternate energyExpand
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