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LOW-SUBSONIC FLIGHT CHRACTERISTICS OF A MODEL OF A SUPERSONIC-AIRPLANE CONFIGURATION WITH A PARAWING A LANDING AID.

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BookPublisher: Nasa, Washington, D.C. 1963Description: 50.DDC classification: NASA | TN D-2031

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-2031 (Browse shelf)	Not for loan		65590

Total holds: 0

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Previous	NASA TN D-2013 FULL-SCALE WIND-TUNNEL TEST OF THE VZ-2 VTOL AIRPLANE WITH PARICULAR REFERENCE TO THE WIND STALL PHENOMENA.	NASA TN D-202 EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF HEAT-TRANSFER CHARACTERISTICS OF A RETURN-FLOW AIR-COOLED TURBINE ROTOR BLADE	NASA TN D-203 EXPERIMENTAL STUDY OF ZERO-FLOW ENJECTORS USING GASEOUS NITROGEN	NASA TN D-2031 LOW-SUBSONIC FLIGHT CHRACTERISTICS OF A MODEL OF A SUPERSONIC-AIRPLANE CONFIGURATION WITH A PARAWING A LANDING AID.	NASA TN D-2032 MAGNETICALLY ROTATED ELECTRIC ARC AIR HEATER EMPLOYING A STRONG MAGNETIC FIELD AND COPPER ELECTRODES.	NASA TN D-2033 TRANSONIC INVESTIGATION OF DYRAMIDAL REENTRY CONFIGURATION WITH CAMBERED VARIABLE-SWEEP WINGS AND VARIOUS LONGITUDINAL CONTROLS.	NASA TN D-2034 SUBSONIC AERODYNAMIC HEAT TRASFER TO A SURFACE RECESSED WITHIN A FORWARD STAGNATION REGION SLIT.	Next

Bound With Nasa Tn D-2032-2040.

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