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AERODYNAMIC CHARACTERISTICS AT LOW SPEED OF A REENTRY6 CONFIGURATION HAVING RIGID RESTRACTABLE CONICAL LIFTING SURFACES

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BookPublisher: Nasa, Washington, D.C. 1960Description: 26.DDC classification: NASA | TN D-622

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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-622 (Browse shelf)	Not for loan		TR12348

Total holds: 0

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Previous	NASA TN D-6217 - SIMPLE INTEGRAL METHOD FOR THE CALCULATION OF REAL-GAS TURBULENT BOUNDARY LAYERS WITH VARIABLE EDGE ENTROPY	NASA TN D-6218 - METHOD FOR REDUCING THE SENSITIVITY OF OPTIMAL NONLINEAR SYSTEM TO PARAMETER UNCERTAINTY	NASA TN D-6219 - ERROR ANALYSIS OF THE MARS GRAVITATIONAL FIELD ESTIMATION USING RANGE AND RANGE -RATE DATA FROM A VIKING-TYPE ORBITER	NASA TN D-622 AERODYNAMIC CHARACTERISTICS AT LOW SPEED OF A REENTRY6 CONFIGURATION HAVING RIGID RESTRACTABLE CONICAL LIFTING SURFACES	NASA TN D-6221 - CALCULATION BY A FINITE-DIFFERENCE METHOD OF SUPERSONIC TURBULENT BOUNDARY LAYERS WITH TANGENTIAL SLOT INJECTION	NASA TN D-6222 - EFFECT OF ENGINE POSITION AND HIGH-LIFT DEVICES ON AERODYNAMIC CHARACTERISTICS OF AN EXTERNAL-FLOW JET-FLAP STOL MODEL	NASA TN D-6223 - SUPERSONIC ASYMMETRIC FLUTTER AND DIVERGENCE OF TRUNCATED CONICAL SHELLS WITH RING-SUPPORTED EDGES	Next

Bound With Nasa Tn D-621 & 623-630

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