Wind Tunnel Investigation Of The High Subsonic Static Longitudinal Stability Characteristics Of Several Wing Body Configurations Designed For High Lift Drag Ratios At A Mach Number Of 14 PDF Download

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Wind-tunnel Investigation of the High-subsonic Static Longitudinal Stability Characteristics of Several Wing-body Configurations Designed for High Lift-drag Ratios at a Mach Number of 1.4

Wind-tunnel Investigation of the High-subsonic Static Longitudinal Stability Characteristics of Several Wing-body Configurations Designed for High Lift-drag Ratios at a Mach Number of 1.4
Author: Paul G. Fournier
Publisher:
Total Pages: 42
Release: 1958
Genre: Stability of airplanes, Longitudinal
ISBN:

Download Wind-tunnel Investigation of the High-subsonic Static Longitudinal Stability Characteristics of Several Wing-body Configurations Designed for High Lift-drag Ratios at a Mach Number of 1.4 Book in PDF, ePub and Kindle

Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel to investigate the high-subsonic static longitudinal stability characteristics and lift-drag ratios of several wing-body models designed to provide high lift-drag ratios at a Mach number of 1.4. The basic configuration had a thin highly swept wing of aspect ratio 2.91 with NACA 65A-series airfoil sections. Other configurations included bodies modified by two types of indentation and two other wings, one wing without camber but with 4 degrees linear twist (washout) and a second wing with both camber and twist.


Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds

Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds
Author: James W. Wiggins
Publisher:
Total Pages: 692
Release: 1956
Genre: Airplanes
ISBN:

Download Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds Book in PDF, ePub and Kindle

An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the horizontal- and vertical-tail contributions to the static lateral stability of a complete-model swept-wing configuration at high subsonic speeds. The results indicate that, in a general, Mach number effects within the range studied and wing effects on the tail contribution were small and the overall trends of the data of the present investigation agreed with those which have been established at low speeds.


Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 388
Release: 1959
Genre: Aeronautics
ISBN:

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Index of NASA Technical Publications

Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 448
Release: 1960
Genre: Aeronautics
ISBN:

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A Selected Listing of NASA Scientific and Technical Reports

A Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
Total Pages: 436
Release: 1968
Genre: Aeronautics
ISBN:

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Index to NASA Technical Publications

Index to NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages:
Release: 1960-07
Genre:
ISBN:

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Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 508
Release: 1954
Genre: Aeronautics
ISBN:

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