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SUPERSONIC AERODYNAMIC CHARACTERISTICS AND SHOCKS STANDOFF DISTANCES FOR LARGE-ANGLE CONES WITH AND WITHOUT CYLINDRICAL AFTERBODIES

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BookPublisher: Nasa, Washington, D.C. 1969Description: 96.DDC classification: NASA | TN D-5334

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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-5334 (Browse shelf)	Not for loan		TR10453

Total holds: 0

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Previous	NASA TN D-5330 - CHARACTERISTICS DESIGN STUDY OF MIXED-COMPRESSION TWO-DIMENSIONAL INLETS WITH LOW-ANGLE COWLS FOR THE MACH NUMBER RANGE 2.70 TO 1.80	NASA TN D-5332 MAGNETOSPHERIC DUCT PROPAGATION RESEARCH USING ALOUETTE-2 TOPSIDE-SOUNDER OBSERVATIONS	NASA TN D-5333 EFFECTS OF JET-EXHAUST LOCATION ON THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A JET V/STOL MODEL.	NASA TN D-5334 SUPERSONIC AERODYNAMIC CHARACTERISTICS AND SHOCKS STANDOFF DISTANCES FOR LARGE-ANGLE CONES WITH AND WITHOUT CYLINDRICAL AFTERBODIES	NASA TN D-5335 A FINITE-STEP METHOD FOR CALCULATION OF THEORETICAL LOAD DISTRIBUTIONS FOR ARBITRARY LIFTING-SURFACE ARRANGEMENTS AT SUBSONIC SPEEDS.	NASA TN D-5336 GASEOUS-HYDROGEN REQUIREMENTS FOR THE DISCHARGE OF LIQUID HYDROGEN FROM A 1.52-METER-(5-FT-) DIAMETER SPHERICAL TANK	NASA TN D-5337 INERCOMPARISON OF THE MINITRACK AND OPTICAL TRACKING NETWORKS USING GEOS 1 LONG-ARC ORBITAL SOLUTIONS.	Next

Bound With: Nasa Tn D-5331-5333,5335-5340

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