Two-dimensional Wind-tunnel Investigation of Sealed 0.22-airfoil-chord Internally Balanced Ailerons of Different Contour on an NACA 65(112)- 213 Airfoil
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AILERONS, BALANCED - INTERNAL↗
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Investigation of an Approximately 0.178-chord-thick NACA 6-series-type Airfoil Section Equipped with Sealed Internally Balanced 0.20-chord Ailerons and with a 0.05-chord Tab
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TABS, AILERON↗
Test of NACA 66,2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane
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WING FLAPS, SLOTTED↗
Wind-tunnel investigation of an NACA 23012 airfoil with two sizes of balanced split flap
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AIRFOILS - NACA 23012 - CHAR , A C , MOMENTS & ORD↗
Wind-tunnel investigation of an NACA 23021 airfoil with two sizes of balanced split flaps
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WING FLAPS - FOWLER↗
Pressure distribution over an airfoil with a balanced split flap
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WING FLAPS, SPLIT - BALANCED↗
Resume of hinge-moment data for unshielded horn- balanced control surfaces
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BIBLIOGRAPHY - CONTROL SURFACES↗
Wind-tunnel investigation of control-surface characteristics III : a small aerodynamic balance of various nose shapes used with a 30-percent-chord flap on an NACA 0009 airfoil
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WING FLAPS - DEFLECTION↗
Wind tunnel investigation of control-surface characteristics XI : various large overhang and internal-type aerodynamic balances for a straight- contour flap on the NACA 0015 airfoil
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WING FLAPS - HINGE MOMENTS↗
Wind-tunnel investigation of control-surface characteristics XXI : medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.40-airfoil-chord flap on an NACA 0009 airfoil
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WING FLAPS-OVERHANG↗
Wind Tunnel Tests of Ailerons at Various Speeds IV : Ailerons of 0.20 Airfoil Chord and True Contour with 0.35 Aileron-chord Extreme Blunt-nose Balance on the NACA 23012 Airfoil
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AILERONS - WIND TUNNEL TESTS↗
Analysis of available data on the effectiveness of ailerons without exposed overhang balance
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LATERAL CONTROL↗
A flight investigation of internally balanced sealed ailerons
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AILERONS, BALANCED - HINGE MOMENTS↗
Calibration of the NASA MC60 Five-Component Semi-span Balance
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wind tunnel balance↗
Rotating Balance Design and Production, GRC-419R
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Force Balance↗
Chapter 13: Software and Methods for Computational Flux Balance Analysis
As genetic engineering of organisms has grown easier and more precise, computational modeling of metabolic systems has played an increasingly important role in both guiding experimental interventions and in understanding the results of metabolic perturbations.
BASIC BIOLOGICAL SCIENCES↗
Power systems balancing with high penetration renewables: The potential of demand response in Hawaii
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29 ENERGY PLANNING, POLICY, AND ECONOMY↗
Stochastic Discontinuous Galerkin Methods (SDGM) based on fluctuation-dissipation balance
Not Available
97 MATHEMATICS AND COMPUTING↗