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Heat Transfer Measurements On A Low Fineness Ratio Cylinder At A Mach Number Of 104 And Angles Of Attack From 0 To 90
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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:
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:
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:
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:
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:
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:
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:
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:
Book Synopsis Temperature Recovery Factors on a Slender 12° Cone-cylinder at Mach Numbers from 3.0 to 6.3 and Angles of Attack Up to 45° by : John O. Reller
Download or read book Temperature Recovery Factors on a Slender 12° Cone-cylinder at Mach Numbers from 3.0 to 6.3 and Angles of Attack Up to 45° written by John O. Reller and published by . This book was released on 1955 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: Temperature recovery factors were determined for a slender, thin-walled cone-cylinder, having a 12° vertex angle and a 1.25-inch-diameter cylinder, at Mach numbers from 3.02 to 6.30. The angle-of-attack range was 0° to 45° at Mach numbers up to 3.50, and about 0° to 20° at Mach numbers from 4.23 to 6.30. A transverse cylinder of the same diameter was also tested at Mach number 3.02. Free-stream Reynolds numbers varied from 1.8 to 11.0 million per foot. Flow visualization studies of boundary-layer transition and flow separation were made and the results correlated with recovery-factor measurements.
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.
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:
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:
Book Synopsis Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44 by :
Download or read book Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44 written by and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 by : Earl A. Price
Download or read book Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 written by Earl A. Price and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
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:
Book Synopsis Turbulent-boundary-layer Heat-transfer and Transition Measurements with Surface Cooling at Mach 6 by : Aubrey M. Cary
Download or read book Turbulent-boundary-layer Heat-transfer and Transition Measurements with Surface Cooling at Mach 6 written by Aubrey M. Cary and published by . This book was released on 1970 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: