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AERODYNAMICS EFFECTS OF MODIFYING WING INBOARD TRAILING-EDGE CAMBER OF A MODEL AT HIGH SUBSONIC SPEEDS.

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BookPublisher: Nasa, Washington, D.C. 1963Description: 43.DDC classification: NASA | TN D-1809

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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-1809 (Browse shelf)	Not for loan		TR15512

Total holds: 0

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Previous	NASA TN D-1801 Maneuver accelerations experienced during routine operations of a commercial turbojet transport airplane [NASA TN D - 1801--TN D-1810]	NASA TN D-1802 FLIGHT OPERATING PROBLEMS AND AERODYNAMIC AND PERFORMANCE CHRACTERISTICS OF A FIXED-WING, TILT-DUCT,VTOL RESEARCH AIRCRAFT.	NASA TN D-1806 INVESTIGATION OF PROPELLER-POWER-PLANT AUTOPRECESSION BOUNDARIES FOR A DYNAMIC-AEROELASTIC MODEL OF A FOUR ENGINE TURBOPROP TRANSPORT AIRPLANE.	NASA TN D-1809 AERODYNAMICS EFFECTS OF MODIFYING WING INBOARD TRAILING-EDGE CAMBER OF A MODEL AT HIGH SUBSONIC SPEEDS.	NASA TN D-1810 VIBRATIONAL-NONEQULIBRIUM FLOW OF NITROGEN IN HYPERSONIC NOZZLES.	NASA TN D-1851 Mass spectrometric investigations of teh atmosphere between 100 and 227 kilometers above wallops island, Virginia [NASA TN D-1851--TN D-1860]	NASA TN D-1871 Evaluation of infrared spectrophotometry for compositional analysis of lunar and planetary soils [NASA TN D-1871--TN D-1880]	Next

Bound With Nasa Tn D-1801-1808,1810.Lack No-1805

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