Heat Transfer Measurements on a Low-fineness- Ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0 Deg to 90 Deg

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Heat Transfer Measurements on a Low-fineness- Ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0 Deg to 90 Deg by :

Download or read book Heat Transfer Measurements on a Low-fineness- Ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0 Deg to 90 Deg written by and published by . This book was released on 1967 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90°

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90° by : Philip E. Everhart

Download or read book Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90° written by Philip E. Everhart and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90°

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (761 download)

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Book Synopsis Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90° by : Philip E. Everhart

Download or read book Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90° written by Philip E. Everhart and published by . This book was released on 1967 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 256 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1968 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50, ̊ 70, ̊ and 90

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ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50, ̊ 70, ̊ and 90 by : James Larry Hunt

Download or read book Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50, ̊ 70, ̊ and 90 written by James Larry Hunt and published by . This book was released on 1969 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50 Degrees, 70 Degrees, and 90 Degrees

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50 Degrees, 70 Degrees, and 90 Degrees by : James L. Hunt

Download or read book Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50 Degrees, 70 Degrees, and 90 Degrees written by James L. Hunt and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Measurements of Aerodynamic Heat Transfer on a 15 Degree Cone-cylinder-flare Configuration in Free Flight at Mach Numbers Up to 4.7

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ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Measurements of Aerodynamic Heat Transfer on a 15 Degree Cone-cylinder-flare Configuration in Free Flight at Mach Numbers Up to 4.7 by : Charles R. Rumsey

Download or read book Measurements of Aerodynamic Heat Transfer on a 15 Degree Cone-cylinder-flare Configuration in Free Flight at Mach Numbers Up to 4.7 written by Charles R. Rumsey and published by . This book was released on 1961 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44

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ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 by : Paige B. Burbank

Download or read book Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 written by Paige B. Burbank and published by . This book was released on 1959 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

U.S. Government Research and Development Reports

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ISBN 13 :
Total Pages : 1152 pages
Book Rating : 4.3/5 (129 download)

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Book Synopsis U.S. Government Research and Development Reports by :

Download or read book U.S. Government Research and Development Reports written by and published by . This book was released on 1967 with total page 1152 pages. Available in PDF, EPUB and Kindle. Book excerpt:

HEAT-TRANSFER AND PRESSURE MEASUREMENTS OF A 1 7-SCALE MODEL OF A MERCURY CAPSULE AT ANGLES OF ATTACK FROM 3 DEG TO & OR - 20 DEG AT MACH NUMBERS OF 3.50 AND 4.44

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ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis HEAT-TRANSFER AND PRESSURE MEASUREMENTS OF A 1 7-SCALE MODEL OF A MERCURY CAPSULE AT ANGLES OF ATTACK FROM 3 DEG TO & OR - 20 DEG AT MACH NUMBERS OF 3.50 AND 4.44 by :

Download or read book HEAT-TRANSFER AND PRESSURE MEASUREMENTS OF A 1 7-SCALE MODEL OF A MERCURY CAPSULE AT ANGLES OF ATTACK FROM 3 DEG TO & OR - 20 DEG AT MACH NUMBERS OF 3.50 AND 4.44 written by and published by . This book was released on 1961 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration

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ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration by : Charles B. Rumsey

Download or read book Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration written by Charles B. Rumsey and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.

Heat Transfer to Bodies at Angles of Attack

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ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Heat Transfer to Bodies at Angles of Attack by : William V. Feller

Download or read book Heat Transfer to Bodies at Angles of Attack written by William V. Feller and published by . This book was released on 1957 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50°, 70°, and 90°

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (249 download)

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Book Synopsis Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50°, 70°, and 90° by : James L. Hunt

Download or read book Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50°, 70°, and 90° written by James L. Hunt and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure and Heat-transfer Measurements on a Mercury Capsule Model

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ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Pressure and Heat-transfer Measurements on a Mercury Capsule Model by : John O. Reller

Download or read book Pressure and Heat-transfer Measurements on a Mercury Capsule Model written by John O. Reller and published by . This book was released on 1962 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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ISBN 13 :
Total Pages : 21 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44 by : Stallings, Jr. (Robert L.)

Download or read book Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44 written by Stallings, Jr. (Robert L.) and published by . This book was released on 1959 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Government Reports Announcements

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ISBN 13 :
Total Pages : 824 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Government Reports Announcements by :

Download or read book Government Reports Announcements written by and published by . This book was released on 1967 with total page 824 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 by : Robert L. O'Neal

Download or read book Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 written by Robert L. O'Neal and published by . This book was released on 1962 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: