Calculations of the supersonic wave drag of nonlifting wings with arbitrary sweepback and aspect ratio : wings swept behind the Mach lines
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Harmon, Sidney M↗
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Results for “WING”
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Stability derivatives of thin rectangular wings at supersonic speeds : wing diagonal ahead of tip mach lines
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Harmon, Sidney M↗
Pitching-moment Derivatives Cmq and Cma at Supersonic Speeds for a Slender-delta-wing and Slender-body Combination and Approximate Solutions for Broad-delta-wing and Slender-body Combinations
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Henderson, Arthur, Jr↗
Commercial airplanes and seaplanes : thick wings or thin wings - all metal or mixed construction
In this report we will consider, as the dominating characteristic, either the load carried, the speed, the radius of action, the fuel consumption, the activity of transport, or, lastly, the qualities of comfort and safety. The first four factors determine the theoretical efficiency, while the others determine its practical efficiency.
COMMERCIAL AIRPLANES - CONSTRUCTION↗
Experimental Investigation of the Low-speed Static and Yawing Stability Characteristics of a 45 Degrees Sweptback High-wing Configuration with Various Twin Vertical Wing Fins
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Goodman, Alex↗
Deflection and stress analysis of thin solid wings of arbitrary plan form with particular reference to delta wings
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Stein, Manuel↗
Deflection of Delta Wings Having a Carry-through-bay Chord Smaller than the Wing Root Chord
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PLATES, STRUCTURAL↗
A simplified mathematical model for calculating aerodynamic loading and downwash for wing-fuselage combinations with wings of arbitrary plan form
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Zlotnick, Martin↗
Calculations of Upwash in the Region Above or Below the Wing-chord Planes of Swept-back Wing-fuselage-nacelle Combinations
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Rogallo, Vernon L↗
Aerodynamics of slender wings and wing-body combinations having swept trailing edges
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Mirels, Harold↗
Wing-body interference at supersonic speeds with an application to combinations with rectangular wings
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Nielsen, Jack N↗
Flight investigation of the effect of transient wing response on wing strains of a four-engine bomber airplane in rough air
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Murrow, Harold N↗
Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees
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Draper, John W↗
Theoretical investigation of the effects upon lift of a gap between wing and body of a slender wing-body combination
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Dugan, Duane W↗
Application of Two-dimensional Vortex Theory to the Prediction of Flow Fields Behind Wings of Wing Body Combinations at Subsonic and Supersonic Speeds
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Rogers, Arthur WM↗
The Effectiveness of Wing Vortex Generators in Improving the Maneuvering Characteristics of a Swept-wing Airplane at Transonic Speeds
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Mcfadden, Norman M↗
An analysis of estimated and experimental transonic downwash characteristics as affected by plan form and thickness for wing and wing-fuselage configurations
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Weil, Joseph↗
Comparison Between Experimental and Predicted Downwash at a Mach Number of 0.25 Behind a Wing-body Combination Having a Triangular Wing of Aspect Ratio of 2.0
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Sorensen, Norman E↗