Technical Abstract Bulletin

Technical Abstract Bulletin
Author :
Publisher :
Total Pages : 1766
Release :
ISBN-10 : UTEXAS:059172131213032
ISBN-13 :
Rating : 4/5 (32 Downloads)

Synopsis Technical Abstract Bulletin by : Defense Documentation Center (U.S.)

Jet Propulsion

Jet Propulsion
Author :
Publisher :
Total Pages : 976
Release :
ISBN-10 : UCAL:$C118777
ISBN-13 :
Rating : 4/5 (77 Downloads)

Synopsis Jet Propulsion by :

Beginning Oct. 1959 some issues include "Russian supplement."

Technical Publications Announcements

Technical Publications Announcements
Author :
Publisher :
Total Pages : 448
Release :
ISBN-10 : PURD:32754084632094
ISBN-13 :
Rating : 4/5 (94 Downloads)

Synopsis Technical Publications Announcements by : United States. National Aeronautics and Space Administration

X-15 Research Results

X-15 Research Results
Author :
Publisher :
Total Pages : 140
Release :
ISBN-10 : UIUC:30112000417359
ISBN-13 :
Rating : 4/5 (59 Downloads)

Synopsis X-15 Research Results by : Wendell H. Stillwell

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

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
Author :
Publisher :
Total Pages : 26
Release :
ISBN-10 : UOM:39015086465922
ISBN-13 :
Rating : 4/5 (22 Downloads)

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

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.