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APOLLO EXPERIENCE REPORT - THE PROBLEM OF STRESS-CORROSION CRACKING

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BookPublisher: Nasa, Washington, D.C. 1973Description: 15.DDC classification: NASA | TN D-7111

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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-7111 (Browse shelf)	Not for loan Untraceable		TR12397

Total holds: 0

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Previous	NASA TN D-7108 - HEATING AND FLOW-FIELD STUDIES ON A STRAIGHT-WING HYPERSONIC REENTRY VEHICLE AT ANGLES OF ATTACK FROM 20[DEGREE] TO 80[DEGREE] WITH SIMULATION OF REAL-GAS TRENDS	NASA TN D-7109 - EFFECT OF REYNOLDS NUMBER AND ENGINE NACELLES ON THE STALLING CHARACTERISTICS OF A MODEL OF A TWIN-ENGINE LIGHT AIRPLANE	NASA TN D-711 INVESTIGATION OF THE STATIC LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS OF A 0.10-SCALE MODEL OF A THREE-STAGE CONFIGURATION OF THE SCOUT RESEARCH VEHICLE AT MACH NUMBERS OF 2.29, 2.96, 3.96	NASA TN D-7111 APOLLO EXPERIENCE REPORT - THE PROBLEM OF STRESS-CORROSION CRACKING	NASA TN D-7112 APOLLO EXPERIENCE REPORT - SIMULATION OF MANNED SPACE FLIGHT FOR CREW TRAINING	NASA TN D-7113 MEASURED CATALYCITIES OF VARIOUS CANDIDATE SPACE SHUTTLE THERMAL PROTECTION SYSTEM COATINGS AT LOW TEMPERATURES	NASA TN D-7114 EXTRACTION OF LONGITUDINAL AERODYNAMIC COEFFICIENTS FROM FORWARD-FLIGHT CONDITIONS OF A TILT WING V/STOL AIRPLANE	Next

Bound With Nasa Tn D-7110, 12-7119.

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