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IMPROVED METHOD FOR DESIGN OF EXPANSION-CHAMBER MUFFLERS WITH APPLICATION TO AN OPERATIONAL HELICOPTER

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BookPublisher: Nasa, Washington, D.C. 1973Description: 71.DDC classification: NASA | TN D-7309 -

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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-7309 - (Browse shelf)	Not for loan		TR9595

Total holds: 0

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Previous	NASA TN D-7305 - EXTENSION OF THE QZ ALGORITHM FOR SOLVING THE GENERALIZED MATRIX EIGENVALUE PROBLEM	NASA TN D-7306 - MODELING OF TURBULENT TRANSPORT IN THE SURFACE LAYER	NASA TN D-7308 - CORRELATION OF NEW HYPERVELOCITY IMPACT DATA BY THRESHOLD PENETRATION RELATIONS	NASA TN D-7309 - IMPROVED METHOD FOR DESIGN OF EXPANSION-CHAMBER MUFFLERS WITH APPLICATION TO AN OPERATIONAL HELICOPTER	NASA TN D-7312 UNSUPERVISED SPATIAL CLUSTERING WITH SPECTRAL DISCRIMINATION	NASA TN D-7313 INTERMEDIATE ENERGY PROTON-DEUTERON ELASTIC SCATTERING	NASA TN D-7314 AN EXPERIMENTAL INVESTIGATION OF A HIGHLY UNDEREXPANDED SONIC JET EJECTING FROM A FLAT PLATE INTO A SUBSONIC CROSSFLOW	Next

Bound With Nasa Tn D-7300-10

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