Related Books

Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings
Language: en
Pages: 40

Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings

Authors: Gaynor J. Adams
Categories: Airplanes
Type: BOOK - Published: 1951 - Publisher:

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The coefficients of damping in roll and rolling effectiveness (with differential incidence of the horizontal surfaces) are determined for a slender, equal-span,
Comparison of High-speed Operating Characteristics of Size 215 Cylindrical-roller Bearings as Determined in Turbojet Engine and in Laboratory Test Rig
Language: en
Pages: 236

Comparison of High-speed Operating Characteristics of Size 215 Cylindrical-roller Bearings as Determined in Turbojet Engine and in Laboratory Test Rig

Authors: Arthur W. Goldstein
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1952 - Publisher:

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Report
Language: en
Pages: 22

Report

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1952 - Publisher:

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NASA Technical Report
Language: en
Pages: 540

NASA Technical Report

Authors:
Categories: Aerodynamics
Type: BOOK - Published: 1964 - Publisher:

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Tests of Two-blade Propellers in the Langley 8-foot High-speed Tunnel to Determine the Effect on Propeller Performance of a Modification of Inboard Pitch Distribution
Language: en
Pages: 724

Tests of Two-blade Propellers in the Langley 8-foot High-speed Tunnel to Determine the Effect on Propeller Performance of a Modification of Inboard Pitch Distribution

Authors: James Benjamin Delano
Categories: Propellers, Aerial
Type: BOOK - Published: 1951 - Publisher:

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This paper presents propeller characteristics for two propellers that differ only in inboard pitch distribution. The forward Mach number range extended to 0.062