Author: Earl D. Knechtel
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
An experimental investigation was conducted to assess the effects of sweep and taper ratio on the longitudinal characteristics of a wing-body combination at Mach numbers from 0.6 to 14 and for a Reynolds number of 1,500,000. The wings were 3 percent thick and of aspect ratio 3. Leading-edge sweep was varied from 19.1 to 53.1 degrees at a constant taper ratio of 0.4, and taper ratio was varied from 0 to 0.5 at a constant sweep angle of 53.1 degrees.
Effects of Sweep and Taper on the Longitudinal Characteristics of an Aspect Ratio 3 Wing-body Combination at Mach Numbers from 0.6 to 1.4
Author: Earl D. Knechtel
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
An experimental investigation was conducted to assess the effects of sweep and taper ratio on the longitudinal characteristics of a wing-body combination at Mach numbers from 0.6 to 14 and for a Reynolds number of 1,500,000. The wings were 3 percent thick and of aspect ratio 3. Leading-edge sweep was varied from 19.1 to 53.1 degrees at a constant taper ratio of 0.4, and taper ratio was varied from 0 to 0.5 at a constant sweep angle of 53.1 degrees.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
An experimental investigation was conducted to assess the effects of sweep and taper ratio on the longitudinal characteristics of a wing-body combination at Mach numbers from 0.6 to 14 and for a Reynolds number of 1,500,000. The wings were 3 percent thick and of aspect ratio 3. Leading-edge sweep was varied from 19.1 to 53.1 degrees at a constant taper ratio of 0.4, and taper ratio was varied from 0 to 0.5 at a constant sweep angle of 53.1 degrees.
Effects of Sweep and Taper Ratio on the Longitudinal Characteristics of an Aspect Ratio 3 Wing-body Combination at Mach Numbers from 0.6 to 1.4
Author: Earl D. Knechtel
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
Book Description
Summary and Analysis of Horizontal-tail Contribution to Longitudinal Stability of Swept-wing Airplanes at Low Speeds
Author: Robert H. Neely
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 96
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 96
Book Description
Subject Index to Unclassified ASTIA Documents
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 894
Book Description
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 894
Book Description
The Theory of Diffusion in Strained Systems
Author: Louis A. Girifalco
Publisher:
ISBN:
Category : Crystals
Languages : en
Pages : 1082
Book Description
A general theory of solid-state diffusion in strained systems is developed on a molecular-kinetic basis. The theory predicts that for simple strains the diffusion coefficient is an exponential function of the lattice parameter and that the rate of change of the diffusion coefficient with strain is linearly related to the interatomic forces. It has also been shown that for plastic flow the diffusion coefficient is a linear function of strain rate. All the conclusions are confirmed by the data available in the literature.
Publisher:
ISBN:
Category : Crystals
Languages : en
Pages : 1082
Book Description
A general theory of solid-state diffusion in strained systems is developed on a molecular-kinetic basis. The theory predicts that for simple strains the diffusion coefficient is an exponential function of the lattice parameter and that the rate of change of the diffusion coefficient with strain is linearly related to the interatomic forces. It has also been shown that for plastic flow the diffusion coefficient is a linear function of strain rate. All the conclusions are confirmed by the data available in the literature.
NASA Technical Report
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 100
Book Description
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Index to NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description