Bauknecht et al., 2017 - Google Patents
Airborne acquisition of blade tip displacements and vortices on a coaxial ultralight helicopterBauknecht et al., 2017
- Document ID
- 8499031926909141253
- Author
- Bauknecht A
- Grebing B
- Raffel M
- Publication year
- Publication venue
- 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
External Links
Snippet
Coaxial, counter-rotating rotor systems allow for the design of compact and light rotorcraft that are easy to pilot in comparison to conventional helicopters. 1 The reduced rotor dimensions, simple controllability, and light weight structure in combination with no need for …
- 238000006073 displacement reaction 0 title description 25
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
- G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
- G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
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