Rules and regulations governing the Fokker Soaring-Flight Contest over water or level land
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Experimental Determination of the Range of Applicability of the Transonic Area Rule for Wings of Triangular Plan Form
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Page, William A↗
The similarity rules for second-order subsonic and supersonic flow
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Van Dyke, Milton D↗
Rules and regulations for endurance contest of aviation engines : under the auspices of the Aero Club of France
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On the range of applicability of the transonic area rule
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Spreiter, John R↗
Provisional rules for the inspection of aircraft adopted by the French Bureau Veritas
These new regulations are intended to replace those of November 1, 1922, and give the directions to be followed in the supervision of aircraft by the agents of the Aeronautical Section of the Bureau Veritas.
INSPECTION - BUREAU VERITAS (FR )↗
A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degree Sweptback-wing-body Combination
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Robinson, Harold L↗
A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination
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Williams, Claude V↗
Preliminary Investigation of the Effects of Body Contouring as Specified by the Transonic Area Rule on the Aerodynamic Characteristics of a Delta Wing-body Combination at Mach Numbers of 1.41 and 2.01
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Carlson, Harry W↗
Development of a supersonic area rule and an application to the design of a wing-body combination having high lift-to-drag ratios
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Whitcomb, Richard T↗
An investigation of the transonic area rule by flight tests of a sweptback wing on a cylindrical body with and without body indentation between Mach numbers 0.9 and 1.8
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Hoffman, Sherwood↗
Application of transonic area rule to a sharp-lipped ducted nacelle
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Walters, Richard E↗
A flight investigation of the transonic area rule for a 52.5 degree sweptback wing-body configuration at Mach numbers between 0.8 and 1.6
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Hoffman, Sherwood↗
On the range of applicability of the transonic area rule
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Spreiter, John R↗
Flight Investigation of the Supersonic Area Rule for a Straight Wing-body Configuration at Mach Numbers Between 0.8 and 1.5
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Hoffman, Sherwood↗
Effect of Wing Size and Amount of Indentation on Applicability of Transonic Area Rule to Swept-wing Configurations
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Hall, James Rudyard↗
Influence of the body flow field on the zero-lift wave drag of wing-body combinations modified in accordance with the transonic area rule
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Page, William A↗
External-store drag reduction at transonic and low supersonic Mach numbers by application of Baldwin's moment-of-area rule
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Levy, Lionel L JR↗