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Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading -edge droop in combination with outboard chord-extensions and notches [NASA TN D-834]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. Nasa 1961Description: 30p.Subject(s): aerodynamicSummary: NASA technical report

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-834 (Browse shelf)	Not for loan		TR16135

Total holds: 0

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Previous	NASA TN D-831 A study of flutter at low mass rations with possible application to hydrofoils [NASA TN D-831]	NASA TN D-832 Investigationsof grain-boundary stress concentrations in silver chloride [NASA TN D-832]	NASA TN D-833 Experimental studies of flutter of buckled rectangular panels at mach numbers from 1.2 to 3.0 including effects of pressure differential and of panel width-length ratio [NASA TN D-833]	NASA TN D-834 Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading -edge droop in combination with outboard chord-extensions and notches [NASA TN D-834]	NASA TN D-835 Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 [NASA TN D-835]	NASA TN D-836 Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket -propelled airplane configuration having a low 52.5 (degree) delta wing and an unswept horizontal tail [NASA TN D-836]	NASA TN D-837 Influence of impurity elements, structure, and prestrain on tensile transition temperature of chromium [NASA TN D-837]	Next

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