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Results for “WINGS - SWEEPBACK”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 505 records · Page 28

All sources NASA NTRS DOE OSTI

NASA NTRS1954

The Effects of Horizontal-tail Height and a Partial-span Leading-edge Extension on the Static Longitudinal Stability of a Wing-fuselage-tail Combination Having a Sweptback Wing

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Bandettini, Angelo↗

NASA NTRS1954

Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing-body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models

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Bland, William M , Jr↗

NASA NTRS1954

Static Longitudinal Stability Characteristics of a Composite-plan-form Wing Model Including Some Comparisons with a 45 Degree Sweptback Wing at Transonic Speeds

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Wolhart, Walter D↗

NASA NTRS1954

Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick, tapered, upswept wing

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English, Roland D↗

NASA NTRS1954

Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane - Longitudinal Stability and Control

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Smith, Willard G↗

NASA NTRS1955

Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane-lateral and Directional Stability

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Wetzel, Benton E↗

NASA NTRS1954

The Effect of Wing Profile on the Transonic Characteristics of Rectangular and Triangular Wings Having Aspect Ratios of 3 : Transonic Bump Technique

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Nelson, Warren H↗

NASA NTRS1955

Longitudinal Stability Characteristics in Maneuvering Flight of the Convair XF-92A Delta-wing Airplane Including the Effects of Wing Fences

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Sisk, Thomas R↗

NASA NTRS1955

Effects of an All-movable Wing-tip Control on the Longitudinal Stability of a 60 Degree Sweptback-wing--indented-body Configuration Equipped with Fences at Transonic Speeds

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Fischetti, Thomas L↗

NASA NTRS1955

Free-flight Investigation to Determine Some Effects of Tail Damping and Wing-tail Interference on the Rolling Effectiveness of Inboard and Outboard Ailerons on an Untapered Sweptback Wing

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English, Roland D↗

NASA NTRS1955

Summary of the Flight Conditions and Maneuvers in which Maximum Wing and Tail Loads Were Experienced on a Swept-wing Fighter Airplane

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Sadoff, Melvin↗

NASA NTRS1955

Investigation of Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail : Basic-data Presentation, M = 2.01

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Spearman, M Leroy↗

NASA NTRS1955

Flight investigation and analysis of the wing deformations of a swept-wing bomber during push-pull maneuvers

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Mayo, Alton P↗

NASA NTRS1955

A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body

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Palmer, William E↗

NASA NTRS1955

Comparison of the static stability of a 68.7 degree delta-wing model with dihedral and a twisted and cambered wing model of the same plan form

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Paulson, John W↗

NASA NTRS1955

Experimental Static Aerodynamic Forces and Moments at Low Speed on a Canard Missle During Simulated Launching from the Midsemispan and Wing-tip Locations of a 45 Degree Sweptback Wing-fuselage Combination

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Alford, William J , Jr↗

NASA NTRS1955

Experimental Investigation of Some Aerodynamic Effects of a Gap Between Wing and Body of a Moderately Slender Wing-body Combination at a Mach Number of 1.4

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Dugan, Duane W↗

NASA NTRS1955

Low-speed Investigation of the Effects of Wing Tanks and Speed Brakes on the Static Stability of a Model Having a 40 Degree Swept Wing

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Sleeman, William C , Jr↗