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FRICTION AND PRESSURE DRAG OF BOUNDARY-LAYER DIVERTER SYSTEMS AT MACH NUMBER OF 3.0

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BookPublisher: Nasa, Washington, D.C. 1960Description: 20.DDC classification: NASA | TM X-147

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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 TM X-147 (Browse shelf)	Not for loan		TR16234

Total holds: 0

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Previous	NASA TM X-138 EFFECTS OF TWIST AND CAMBER AND THICKNESS ON THE AERODYNAMIC CHARACTERISTICS OF A75 (DEGRE) SWEPT ARROW WING AT A MACH NUMBER OF 2.91	NASA TM X-141 STATIC STABILITY CHARACTERISTICS OF THREE THICK WING MODELS WITH PARABOLIC PLAN FORMS AT A MACH NUMBER OF 3.11	NASA TM X-144 LOW-SPEED MEASUREMENTS OF OSCILLATORY LATERAL STABILITY DERIVATIVES OF A 1/7-SCALE MODEL OF THE NORTH AMERICAN X-15 AIRPLANE	NASA TM X-147 FRICTION AND PRESSURE DRAG OF BOUNDARY-LAYER DIVERTER SYSTEMS AT MACH NUMBER OF 3.0	NASA TM X-149 FERFORMANCE SUMMARY AND ANALYSIS OF A MACH 3.0 DESIGN AXISYMMETRIC ALL-EXTERNAL -COMPRESSION DOUBLE-CONE INLET FROM MACH NUMBER 3.0 TO 0.8	NASA TM X-151 MIXING CHARACTERISTICS DOWNSTREAM OF CORE REGION OF HIGH-TEMPERATURE AXISYMMETRIC JETS EXHAUSTING INTO TRANSONIC AND SUPERSONIC STREAMS	NASA TM X-154 PERFORMANCE OF A MACH NUMBER 3.0 DESIGN AXISYMMETRIC DOUBLE-CONE EXTERNAL-COMPRESSION INLET IN THE MACH NUMBER RANGE 1.97 TO 0.79	Next

Bound With Nasa Tm X-130-144,149-156,Lack No.131-34,39-40,42-43,45-46,48-50,52-53,55

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