Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44
| Title | Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 PDF eBook |
| Author | Paige B. Burbank |
| Publisher | |
| Pages | 30 |
| Release | 1959 |
| Genre | Aerodynamic heating |
| ISBN |
Download Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 Book in PDF, Epub and Kindle
Heat-transfer and Pressure Measurements on Flat-face Cylinder at Mach Number Range of 2.49 to 4.44 [with List of References]
| Title | Heat-transfer and Pressure Measurements on Flat-face Cylinder at Mach Number Range of 2.49 to 4.44 [with List of References] PDF eBook |
| Author | |
| Publisher | |
| Pages | 24 |
| Release | 1959 |
| Genre | |
| ISBN |
Download Heat-transfer and Pressure Measurements on Flat-face Cylinder at Mach Number Range of 2.49 to 4.44 [with List of References] Book in PDF, Epub and Kindle
Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44
| Title | Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44 PDF eBook |
| Author | Stallings, Jr. (Robert L.) |
| Publisher | |
| Pages | 21 |
| Release | 1959 |
| Genre | Aerodynamic measurements |
| ISBN |
Download Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44 Book in PDF, Epub and Kindle
Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44
| Title | Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 PDF eBook |
| Author | Paige B. Burbank |
| Publisher | |
| Pages | 430 |
| Release | 1962 |
| Genre | Heat |
| ISBN |
Download Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 Book in PDF, Epub and Kindle
Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90°
| Title | Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90° PDF eBook |
| Author | Philip E. Everhart |
| Publisher | |
| Pages | 44 |
| Release | 1967 |
| Genre | Airplanes |
| ISBN |
Download Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90° Book in PDF, Epub and Kindle
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
| Title | 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 PDF eBook |
| Author | |
| Publisher | |
| Pages | 50 |
| Release | 1967 |
| Genre | |
| ISBN |
Download 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 Book in PDF, Epub and Kindle
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
| Title | 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 PDF eBook |
| Author | Charles B. Rumsey |
| Publisher | |
| Pages | 26 |
| Release | 1955 |
| Genre | Aerodynamic heating |
| ISBN |
Download 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 Book in PDF, Epub and Kindle
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.