Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44

Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44
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Total Pages : 26
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ISBN-10 : NASA:31769000459241
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44 by :

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Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44 Related Books

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Abstract: The concave-nose stagnation-point heating is 40 percent of that of a hemisphere nose shape having the same diameter. At angles of attack of ℗±5© a
Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44
Language: en
Pages: 21
Authors: Stallings, Jr. (Robert L.)
Categories: Aerodynamic measurements
Type: BOOK - Published: 1959 - Publisher:

GET EBOOK