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LOADS INDUCED ON A FLAT PLATE AT A MACH NUMBER OF 4.5 WITH A SONIC OR SUPERSONIC JET EXHAUSTING NORMAL TO THE SURFACE

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BookPublisher: Nasa, Washington, D.C. 1963Description: 24.DDC classification: NASA | TN D-1935 -

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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-1935 - (Browse shelf)	Not for loan		TR10209

Total holds: 0

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Previous	NASA TN D-1932 - FREE-FLIGHT INVESTIGATION OF THE DEPLOYMENT, DYNAMIC STABILITY, AND CONTROL CHARACTERISTICS OF A 1/12-SCALE DYNAMIC RADIO-CONTROLLED MODEL OF A LARGE BOOSTER AND PARAWING	NASA TN D-1933 - EFFECT OF FABRICATION-TYPE SURFACE ROUGHNESS ON TRANSITION ON OGIVE-CYLINDER MODELS AT MACH NUMBERS OF 1.61 AND 2.01	NASA TN D-1934 - INVESTIGATION OF THE LANDING CHARACTERISTICS OF A REENTRY VEHICLE HAVING CANTED MULTIPLE-AIR-BAG LOAD-ALLEVIATION SYSTEM	NASA TN D-1935 - LOADS INDUCED ON A FLAT PLATE AT A MACH NUMBER OF 4.5 WITH A SONIC OR SUPERSONIC JET EXHAUSTING NORMAL TO THE SURFACE	NASA TN D-1936 - TRAILBLAZER I REENTRY-BODY WIND-TUNNEL TESTS AT A MACH NUMBER OF 6.7 WITH THEORETICAL AERODYNAMICS AND A LIMITED DYNAMIC ANALYSIS	NASA TN D-1937 - LOW-SPEED INVESTIGATION OF CABLE TENSION AND AERODYNAMIC CHARACTERISTICS OF A PARAWING AND SPACECRAFT COMBINATION	NASA TN D-1938 - TRAJECTORY ANALYSIS OF A VARIABLE-DRAG PAYLOAD EJECTED FROM A VEHICLE IN A LOW EARTH ORBIT	Next

Bound With Nasa Tn D-1931-40

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