Charts for Estimating Rotor-blade Flapping Motion of High-performance Helicopters

Charts for Estimating Rotor-blade Flapping Motion of High-performance Helicopters
Author :
Publisher :
Total Pages : 692
Release :
ISBN-10 : STANFORD:36105024832060
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Charts for Estimating Rotor-blade Flapping Motion of High-performance Helicopters by : Robert J. Tapscott

Download or read book Charts for Estimating Rotor-blade Flapping Motion of High-performance Helicopters written by Robert J. Tapscott and published by . This book was released on 1956 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: Theoretically derived charts showing steady-state and first- and second-harmonic flapping coefficients are presented for helicopter rotors having hinged rectangular blades with a linear twist of 0, -8, and -16 degrees. The charts, showing the rotor flapping coefficients for combinations of inflow ratio and blade pitch angle, are presented for tip-speed ratios ranging from 0.05 to 0.50.


Charts for Estimating Rotor-blade Flapping Motion of High-performance Helicopters Related Books

Charts for Estimating Rotor-blade Flapping Motion of High-performance Helicopters
Language: en
Pages: 692
Authors: Robert J. Tapscott
Categories: Charts, diagrams, etc
Type: BOOK - Published: 1956 - Publisher:

DOWNLOAD EBOOK

Theoretically derived charts showing steady-state and first- and second-harmonic flapping coefficients are presented for helicopter rotors having hinged rectang
Rotorcraft Aeromechanics
Language: en
Pages: 949
Authors: Wayne Johnson
Categories: Mathematics
Type: BOOK - Published: 2013-04-29 - Publisher: Cambridge University Press

DOWNLOAD EBOOK

A rotorcraft is a class of aircraft that uses large-diameter rotating wings to accomplish efficient vertical take-off and landing. The class encompasses helicop
Technical Note - National Advisory Committee for Aeronautics
Language: en
Pages: 386
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1956 - Publisher:

DOWNLOAD EBOOK

Technical Note
Language: en
Pages: 348
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1956 - Publisher:

DOWNLOAD EBOOK

Analysis of Wind-tunnel Tests to a Mach Number of 0.90 of a Four-engine Propeller-driving Airplane Configuration Having a Wing with 40 Degrees Sweepback and an Aspect Ratio of 10
Language: en
Pages: 658
Authors: George G. Edwards
Categories: Aerodynamics
Type: BOOK - Published: 1956 - Publisher:

DOWNLOAD EBOOK

An investigation has been conducted at speeds up to a Mach number of 0.90 to determine the effects of operating propellers on the longitudinal characteristics o