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Free-flight aerodynamic-heating data to mach number 10.4 for a modified von karman nose shape [NASA TN D-889]

By: Bland, William M.

Contributor(s): Collie, Katherine A.

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Nasa Washington 1961Description: 28p.Subject(s): Free-fligh

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NASA technical report

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-889 (Browse shelf)	Not for loan		TR65489(h)

Total holds: 0

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Previous	NASA TN D-886 Theory of an electromagnetic mass accelerator for achieving hypervelocities [NASA TN D-886]	NASA TN D-887 . Effects of boattailing and nozzle extension on the thrust-minus-drag of a multiple-jet configuration [NASA TN D-887]	NASA TN D-888 Measurements of aerodynamic heat transfer and boundary-layer transition on a 15 deg. cone in free flight at supersonic mach numbers up to 5.2 [NASA TN D-888]	NASA TN D-889 Free-flight aerodynamic-heating data to mach number 10.4 for a modified von karman nose shape [NASA TN D-889]	NASA TN D-890 Simple formulas for stagnation-point convective heat loads in lunar return [NASA TN D-890]	NASA TN D-951 Supersonic free-flight measurement of heat transfer and transition on 10 cone having a low temperature ratio.[TN D-951-TN D-960]	NASA TN F-261 THE PROBLEM OF THE CONVERGENCE OF THE METHOD OF INTEGRAL RATIOS	Next

NASA technical report

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