NASA technical notes. D-642. Effect of shock impingement on distribution of heat-transfer coefficients on right circular cylinder at Mach numbers of 2.65, 3.51, and 4.44 [with list of references]; by Robert A. Newlander.
Publication Title:
Effect of shock impingement on distribution of heat-transfer coefficients on right circular cylinder at Mach numbers of 2.65, 3.51, and 4.44 [with list of references]; by Robert A. Newlander.
Display Title:
NASA technical notes. D-642. Effect of shock impingement on distribution of heat-transfer coefficients on right circular cylinder at Mach numbers of 2.65, 3.51, and 4.44 [with list of references]; by Robert A. Newlander.
Series Title:
NASA technical notes.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Newlander, Robert A.
Date:
Jan. 1961
Publish Date ISO Format:
1961-01-01T00:00:00Z
Publication Start:
19610101
Publication End:
19610131
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
12
Publication year:
1961
SuDoc number:
NAS 1.14:D-(nos.)
Description:
cover title, 28+ [4] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] Φ For Sale by OTS, Commerce Dept. Paper, 75c.