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A WIND-TUNNEL INVESTIGATION OF A TRANSONIC-TRANSPORT CONFIGURATION UTILIZING DRAG-REDUCING DEVICES AT MACH NUMBERS FROM 0.20 TO 1.03 [NASA TN D-636]

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BookPublisher: Washington, D.C. National Aeronautics and Space Administration 1961Description: 117p.Subject(s): Wind tunnel

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-631-640	Not for loan		TR12765 [D-636]

Total holds: 0

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Previous	AN ANALYSIS OF THE FLAPWISE BENDING FREQUENCIES MODE SHAPES OF ROTOR BLADES HAVING TWO FLAPPING HINGES TO REDUCE VIBRATION LEVELS [NASA TN D-633]	EFFECTS OF CONE ANGLE, MACH NUMBER, AND NOSE BLUNTING ON TRANSITION AT SUPERSONIC SPEEDS [NASA TN D-634]	FATIGUE INVESTIGATION OF FULL-SCALE WING PANELS OF 7075 ALUMINUM ALLOY [NASA TN D-635]	A WIND-TUNNEL INVESTIGATION OF A TRANSONIC-TRANSPORT CONFIGURATION UTILIZING DRAG-REDUCING DEVICES AT MACH NUMBERS FROM 0.20 TO 1.03 [NASA TN D-636]	WIND-TUNNEL INVESTIGATION OF THE EFFECTS OF WING BODIES, FENCES, FLAPS AND A FUSELAGE ADDITION ON THE WING BUFFET RESPONSE OF A TRANSONIC TRANSPORT MODEL [NASA TN D-637]	ROCKET-MODEL INVESTIGATION OF LATERAL-STABILITY CHARACTERISTICS AND POWER EFFECTS OF A JET-ENGINE AIRPLANE CONFIGURATION WITH TAIL BOOM AT MACH NUMBERS FROM 1.15 TO 1.37 [NASA TN D-638]	EXPERIMENTAL STUDY OF A SINGLE-COIL INDUCED-ELECTROMOTIVE-FORCE PLASMA ACCELERATOR [NASA TN D-639]	Next

Bound vol. contains NASA TN D 631-640

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