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THE SHOCK-WAVE PATTERNS ON A CRANKED-WING CONFIGURATION

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BookPublisher: Nasa, Washington, D.C. 1960Description: 12.DDC classification: NASA | TN D-346 -

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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-346 - (Browse shelf)	Not for loan Untraceable		TR10409

Total holds: 0

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Previous	NASA TN D-343 - SELF-ADAPTIVE MISSILE GUIDENCE SYSTEM FOR STATISTICAL INPUTS	NASA TN D-344 - EXPERIMENTAL DETERMINATION OF THE PRESSURE DISTRIBUTION ON A RECTANGULAR WING OSCILLATING IN THE FIRST BENDING MODE FOR MACH NUMBERS FROM 0.24 TO 1.30	NASA TN D-345 - PHYSIOLOGICAL EFFECTS OF ACCELERATION OBSERVED DURING A CENTRIFUGE STUDY OF PILOT PERFORMANCE	NASA TN D-346 - THE SHOCK-WAVE PATTERNS ON A CRANKED-WING CONFIGURATION	NASA TN D-3462 - NEWTONIAN AERODYNAMIC CHARACTERISTICS OF BLUNTED RIGHT ELLIPTICAL CONES FOR CONE THICKNESS RATIO OF 0.25 TO 3	NASA TN D-3463 - REVISED THREE DEGREE OF FREEDOM PARTICLE TRAJECTORY PROGRAM CO3E FOR THE IBM 7094 COMPUTER	NASA TN D-3464 - ITERATIVE METHOD FOR COMPUTING THE GENERALIZED INVERSE OF A MATRIX	Next

Bound With Nasa Tn D-341-50

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