Cite
Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 deg to 180 deg
MLA
Lamb, M., and R. L. Stallings Jr. Heat-Transfer Distributions on a 0.013-Scale Shuttle Solid Rocket Booster at Mach 3.70 and Angles of Attack from 0 Deg to 180 Deg. Nov. 1976. EBSCOhost, widgets.ebscohost.com/prod/customlink/proxify/proxify.php?count=1&encode=0&proxy=&find_1=&replace_1=&target=https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&scope=site&db=edsnas&AN=edsnas.19770004052&authtype=sso&custid=ns315887.
APA
Lamb, M., & Stallings, R. L., Jr. (1976). Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 deg to 180 deg.
Chicago
Lamb, M, and R. L. Stallings Jr. 1976. “Heat-Transfer Distributions on a 0.013-Scale Shuttle Solid Rocket Booster at Mach 3.70 and Angles of Attack from 0 Deg to 180 Deg,” November. http://widgets.ebscohost.com/prod/customlink/proxify/proxify.php?count=1&encode=0&proxy=&find_1=&replace_1=&target=https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&scope=site&db=edsnas&AN=edsnas.19770004052&authtype=sso&custid=ns315887.