In Flight Transition Measurement On A 100 Cone At Mach Numbers From 05 To 20
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Author | : David F. Fisher |
Publisher | : |
Total Pages | : 148 |
Release | : 1982 |
Genre | : Boundary layer |
ISBN | : |
Download In-flight Transition Measurement on a 100 Cone at Mach Numbers from 0.5 to 2.0 Book in PDF, Epub and Kindle
Author | : David F. Fisher |
Publisher | : |
Total Pages | : |
Release | : 1982 |
Genre | : |
ISBN | : |
Download In-flight Transition Measurement on a 10 O Cone at Mach Numbers from 0.5 to 2.0 Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 148 |
Release | : 1982 |
Genre | : |
ISBN | : |
Download In-flight Transition Measurement on a 10 Deg Cone at Mach Numbers from 0.5 to 2.0 Book in PDF, Epub and Kindle
Author | : David F. Fisher |
Publisher | : |
Total Pages | : 140 |
Release | : 1982 |
Genre | : Boundary layer |
ISBN | : |
Download In-flight Transition Measurement on a 10° Cone at Mach Numbers from 0.5 to 2.0 Book in PDF, Epub and Kindle
Author | : Jerome D. Julius |
Publisher | : |
Total Pages | : 32 |
Release | : 1959 |
Genre | : Heat |
ISBN | : |
Download Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 Book in PDF, Epub and Kindle
Author | : Charles F. Merlet |
Publisher | : |
Total Pages | : 28 |
Release | : 1961 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Supersonic Free-flight Measurements of Heat Transfer and Transition on a 10° Cone Having a Low Temperature Ratio Book in PDF, Epub and Kindle
Heat-transfer coefficients in the form of Stanton number and boundary-layer transition data were obtained from a free-flight test of a 100-inch-long 10° total-angle cone with a 1/16-inch tip radius which penetrated deep into the region of infinite stability of laminar boundary layer over a range of wall-to-local-stream temperature radius and for local Mach numbers from 1.8 to 3.5. Experimental heat-transfer coefficients, obtained at Reynolds numbers up to 160 x 106, were in general somewhat higher than theoretical values. A maximum Reynolds number of transition of only 33 x 106 was obtained. Contrary to theoretical and some other experimental investigations, the transition Reynolds number initially increased while the wall temperature ratio increased at relatively constant Mach number. Further increases in wall temperature ratio were accompanied by a decrease in transition Reynolds number. Increasing transition Reynolds number with increasing Mach number was also indicated at a relatively constant wall temperature ratio.
Author | : |
Publisher | : |
Total Pages | : 734 |
Release | : 1961 |
Genre | : Aeronautics |
ISBN | : |
Download NASA Technical Note Book in PDF, Epub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 448 |
Release | : 1960 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NASA Technical Publications Book in PDF, Epub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 208 |
Release | : 1959 |
Genre | : |
ISBN | : |
Download Index to NASA Technical Publications Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 218 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, Epub and Kindle