Effect of chordwise location of maximum thickness on the supersonic wave drag of sweptback wings
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WINGS, SWEPTBACK↗
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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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Approximate method for predicting form and location of detached shock waves ahead of plane or axially symmetric bodies
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FLOW - DUCTS↗
Data on shape and location of detached shock waves on cones and spheres
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THEORIES - SHOCK WAVES↗
Investigation of 75-millimeter-bore Cylindrical Roller Bearings at High Speeds II : Lubrication Studies - Effect of Oil-inlet Location, Angle, and Velocity for Single-jet Lubrication
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BEARINGS, ROLLER↗
A flight investigation of the effect of center-of-gravity location on gust loads
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Funk, Jack↗
Location of Center of Pressure of Airplane Wings
Data obtained in the Gottingen Aerodynamic Laboratory give considerable detail on the resulting air force moment exerted on various wing sections at different angles of attack. The Gottingen data can serve well to test the hydrodynamic theory, which (on the assumption of uniform motion and hence of infinitely wide wings) renders it possible to compute this moment as a function of the angle of attack. The Gottigen data can well serve to test the theory and it may be noted that experiment and computation compare favorably.
WINGS↗
Effect of horizontal-tail span and vertical location on the aerodynamic characteristics of an unswept tail assembly in sideslip
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Riley, Donald R↗
The effect of longitudinal stiffeners located on one side of a plate on the compressive buckling stress of the plate-stiffener combination
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Seide, Paul↗
A method of deriving frequency-response data for motion of the center of gravity from data measured on an aircraft at locations other than the center of gravity
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Eggleston, John M↗
Investigation of Jet-engine Noise Reduction by Screens Located Transversely Across the Jet
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Callaghan, Edmund E↗
Investigation by the Transonic-bump Method of a 35 Degree Sweptback Semispan Model Equipped with a Flap Operated by a Series of Servovanes Located Ahead of and Geared to the Flap
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Phillips, William H↗
An Investigation of Forward-located Fixed Spoilers and Deflectors as Gust Alleviators on an Unswept-wing Model
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Croom, Delwin R↗
Some Effects of Propeller Operation and Location on Ability of a Wing with Plain Flaps to Deflect Propeller Slipstreams Downward for Vertical Take-off
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Draper, John W↗
The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3. I : Effects of Horizontal-tail Location and Size on the Longitudinal Characteristics
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Tinling, Bruce E↗
Effect of Propeller Location and Flap Deflection on the Aerodynamic Characteristics of a Wing-propeller Combination for Angles of Attack from 0 Degrees to 80 Degrees
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Newsom, William A , Jr↗
Some Ground Measurements of the Forces Applied by Pilots to a Side-located Aircraft Controller
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Brissenden, Roy F↗
Wind-tunnel Investigation of Effects of Spoiler Location, Spoiler Size, and Fuselage Nose Shape on Directional Characteristics of a Model of a Tandem-rotor Helicopter Fuselage
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Williams, James L↗
Pressure Distributions at Transonic Speeds for Slender Bodies Having Various Axial Locations of Maximum Diameter
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Mcdevitt, John B↗