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WIND-TUNNEL INVESTIGATION OF THE LOW-SPEED HIOGH-LEFT AERODYNAMICS OF A ONE-FIFTH SCALE VARIABLE-SWEEP SUPERSONIC TRANSPORT.

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BookPublisher: Nasa, Washington, D.C. 1968Description: 124.DDC classification: NASA | TN D-4844

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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-4844 (Browse shelf)	Not for loan		TR13316

Total holds: 0

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Previous	NASA TN D-484 TELEMETRY CODE AND CLAIBRATIONS FOR SATELLITE 1959 10TA	NASA TN D-4842 A SYNTHESIS OF HUMAN RESPONSE IN CLOSED-LOOP TRACKING TASKS.	NASA TN D-4843 TRANSONIC AERODYNAMIC CHRACTERISTICS OF POWERED MODELS OF SEVERAL APOLLO LAUNCH-ESCAPE VEHICLE CONFIGURATIONS.	NASA TN D-4844 WIND-TUNNEL INVESTIGATION OF THE LOW-SPEED HIOGH-LEFT AERODYNAMICS OF A ONE-FIFTH SCALE VARIABLE-SWEEP SUPERSONIC TRANSPORT.	NASA TN D-4845 EFFECTS OF EDGE CONSTRAINTS ON OPTICAL QUALITIES OF A SPACERCRAFT WINDOW.	NASA TN D-4846 ANALYSIS OF THE AEROELASTIC DIVERGENCE OF TWO EXPERIMENTAL UNGUIDED LAUNCH VECHICLES.	NASA TN D-4848 CENTAUR LAUNCH VEHICLE PROPELLANT UTILIZATION SYSTEM.	Next

Bound With Nasa Tn D-4841-4843,4845-4850.

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