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PERFORMANCE OF A MACH NUMBER 3.0 DESIGN AXISYMMETRIC DOUBLE-CONE EXTERNAL-COMPRESSION INLET IN THE MACH NUMBER RANGE 1.97 TO 0.79

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BookPublisher: Nasa, Washington, D.C. 1960Description: 29.DDC classification: NASA | TM X-154

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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-154 (Browse shelf)	Not for loan		TR16237

Total holds: 0

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Previous	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	NASA TM X-156 AN EXPERIMENTAL INVESTIGATION AT MACH NUMBERS FROM 2.1 TO 3.0 OF CIRCULAR INTERNAL-COMPRESSION INLETS HAVING TRANSLATABLE CENTERBODIES AND PROVISIONS FOR BOUNDARY-LAYER REMOVAL	NASA TM X-16 AN INVESTIGATION OF A 0.05-SCALE MODEL OF THE XSM-64A NAVAHO MISSILE AND BOOSTER AT SUPERSONIC MACH NUMBERS	NASA TM X-167 - STATIC STABILITY CHARACTERISTICS OF A SERIES OF HYPERSONIC BOOST-GLIDE CONFIGURATIONS AT MACH NUMBERS OF 1.41 AND 2.01	Next

Bound With Nasa Tm X-130-151,156,Lack No.Lack No. 131-34,39-40,42-43,45-46,48-50,52-53,55

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