Author: Harry L. Runyan
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36
Book Description
The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented in this report. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter.
Single-degree-of-freedom-flutter Calculations for a Wing in Subsonic Potential Flow and Comparison with an Experiment
Author: Harry L. Runyan
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36
Book Description
The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented in this report. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36
Book Description
The effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented in this report. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter.
Comparison of High-speed Operating Characteristics of Size 215 Cylindrical-roller Bearings as Determined in Turbojet Engine and in Laboratory Test Rig
Author: Arthur W. Goldstein
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 236
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 236
Book Description
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 30
Book Description
Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1208
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1208
Book Description
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1308
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1308
Book Description
Fatigue Strengths of Aircraft Materials
Author: Horace John Grover
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 716
Book Description
This report presents of axial-load fatigue tests on notched specimens of 24S-T3 and 75S-T6 aluminum alloys and normalized SAE 4130 steel with stress-concentration factors of 2.0 (central-circular hole, symmetrical edge notches, and fillets) and 4.0 (symmetrical edge notches and fillets). Fatigue tests were run at several levels of nominal mean stress. Results are compared with previous data for unnotched specimens.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 716
Book Description
This report presents of axial-load fatigue tests on notched specimens of 24S-T3 and 75S-T6 aluminum alloys and normalized SAE 4130 steel with stress-concentration factors of 2.0 (central-circular hole, symmetrical edge notches, and fillets) and 4.0 (symmetrical edge notches and fillets). Fatigue tests were run at several levels of nominal mean stress. Results are compared with previous data for unnotched specimens.
An Introduction to the Theory of Aeroelasticity
Author: Y C Fung
Publisher: Courier Dover Publications
ISBN: 0486469360
Category : Technology & Engineering
Languages : en
Pages : 516
Book Description
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
Publisher: Courier Dover Publications
ISBN: 0486469360
Category : Technology & Engineering
Languages : en
Pages : 516
Book Description
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
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:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 286
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 286
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
Book Description