Spanwise loading for wings and control surfaces of low aspect ratio
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WINGS - CHARACTERISTICS↗
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Results for “DOWNWASH”
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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Linearized lifting-surface theory for swept-back wings with slender plan forms
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THEORIES - AIRFOILS - LIFTING-SURFACE↗
Effect of an Unswept Wing on the Contribution of Unswept-tail Configuration to the Low-speed Static and Rolling-stability Derivatives of a Midwing Airplane Model
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SIDEWASH↗
The spanwise distribution of lift for minimum induced drag of wings having a given lift and a given bending moment
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THEORIES - WINGS↗
Applications of Von Karman's integral method in supersonic wing theory
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WINGS, SWEPTBACK & SWEPTFORWARD↗
The balance of moments and the static longitudinal stability of airplanes
A nomogram is developed which renders it possible by drawing a few lines, to determine: the location of the center of gravity for zero wing and tail moments; the longitudinal dihedral angle; the tail coefficient F(sub h) iota/F(sub t). Moreover there is no difficulty in determining the magnitude of the restoring moment or of the unstable moment.
STABILITY↗
Effect of propeller operation on the pitching moments of single-engine monoplanes
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AIRPLANES - NORTH AMERICAN BT-9B WIND TUNNEL TESTS↗
Determination of the stability and control characteristics of airplanes from tests of powered models
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AIRPLANES - TRIM↗
Full-Scale Tunnel Investigation of the Control and Stability of a Twin-Engine Monoplane with Propellers Operating
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LIFT, DRAG & PITCHING MOMENTS - MONOPLANES↗
Notes on the propeller and slipstream in relation to stability
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STABILITY↗
The Effect of Propeller Operation on the Air Flow in the Region of the Tail Plane for a Twin-engine Tractor Monoplane
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PROPELLERS, TANDEM↗
Jet-boundary corrections to a yawed model in a closed rectangular wind tunnel
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VORTICES - WINGS↗
Air-Flow Surveys in the Region of the Tail Surfaces of a Single-Engine Airplane Equipped with Dual-Rotating Propellers
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PROPELLERS - WIND TUNNEL TESTS↗
Jet-boundary corrections for reflection-plane models in rectangular wind tunnels
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WIND TUNNELS - NACA (10'X7')↗
Charts for determining jet-boundary corrections for complete models in 7- by 10-foot closed rectangular wind tunnels
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DOWNWASH↗
Effect of ground on characteristics of model of a low-wing airplane with full-span slotted flap with and without power
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WING FLAPS, SLOTTED- FULL-SPAN↗
Theoretical distribution of load over a swept-back wing
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LOAD DISTRIBUTION, CHORDWISE - WINGS↗
An Electromagnetic-Analogy Method of Solving Lifting-Surface-Theory Problems
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THEORIES - AIRFOILS - LIFTING-SURFACE↗