Wind-tunnel Investigation at Mach Numbers from 0.8 to 1.4 of Static Longitudinal and Lateral-directional Characteristics of an Unswept-wing Airplane Model PDF Download
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Author: James L. Summers
Publisher:
ISBN:
Category :
Languages : en
Pages : 99
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Book Description
Author: James L. Summers
Publisher:
ISBN:
Category :
Languages : en
Pages : 99
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1056
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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Author: Defense Documentation Center (U.S.)
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ISBN:
Category : Science
Languages : en
Pages : 308
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Book Description
Author: Byron M. Jaquet
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ISBN:
Category : Airplanes
Languages : en
Pages : 24
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Book Description
An investigation was made in the Langley stability tunnel to determine the effects of ventral fins at two positions (zero and -70 degrees dihedral) on the lateral stability derivatives of a 45 degrees swept high-wing model oscillating in yaw. The effect of the ventral fins on the stability derivatives was determined with and without the vertical and horizontal tails for an angle-of-attack range of zero to 30 degrees at a Mach number of 0.13 and a Reynolds number of 830,000, based on the wing mean aerodynamic chord. The steady-state derivatives for a similar model without ventral fins are also presented. No discussion of the data has been made in order to expedite their publication.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
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Author: Paul E. Purser
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 26
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Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like configurations flown as rocket models for other purposes, at transonic speeds, have been collected and compared with the available subsonic and supersonic wind-tunnel data for the same configurations.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 960
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 590
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