The Effect Of Blade Section Thickness Ratios On The Aerodynamic Characteristics Of Related Full Scale Propellers At Mach Numbers Up To 065

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The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65

Author	: A. J. Eggers
Publisher	:
Total Pages	: 286
Release	: 1953
ISBN-10	: OSU:32435065612293
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65 by : A. J. Eggers

Download or read book The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65 written by A. J. Eggers and published by . This book was released on 1953 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65 Related Books

Language: en
Pages: 286

The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65

Authors: A. J. Eggers

Categories: Aerodynamics, Supersonic

Type: BOOK - Published: 1953 - Publisher:

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The Effect of Simulated Icing on Propeller Performance

Authors: Blake W. Corson

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Tests of a 10-foot-diameter three-blade Curtiss 89301-15 propeller with Clark Y blade sections have been conducted in the Langley 16-foot high-speed tunnel in o

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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

Authors: George G. Edwards

Categories: Aerodynamics

Type: BOOK - Published: 1956 - Publisher:

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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

Language: en
Pages: 44

An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47© Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel

Authors: Ralph P. Bielat

Categories: Aerodynamics, Transonic

Type: BOOK - Published: 1951 - Publisher:

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Four wing-body combinations of the same plan form (47 degree sweep, 3.5 aspect ratio, and 0.2 taper ratio) were compared at transonic speeds in the Langley 8-fo

Language: en
Pages: 34

Investigation of the NACA-4-(3)(08)-03 Two-blade Propeller at Forward Mach Numbers to 0.925

Authors: James B. Delano

Categories: Charts, diagrams, etc

Type: BOOK - Published: 1949 - Publisher:

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An investigation of the NACA-4-(3)(08)-03 two-blade propeller has been made in the Langley 8-foot high-speed tunnel for blade angles of 55, 60, and 65 degrees a