Cite
Performance of a single-stage transonic compressor with a blade-tip solidity of 1.5 and comparison with 1.3 and 1.7 solidity stages
MLA
Osborn, W. M., et al. Performance of a Single-Stage Transonic Compressor with a Blade-Tip Solidity of 1.5 and Comparison with 1.3 and 1.7 Solidity Stages. Nov. 1973. 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.19740002621&authtype=sso&custid=ns315887.
APA
Osborn, W. M., Urasek, D. C., & Moore, R. D. (1973). Performance of a single-stage transonic compressor with a blade-tip solidity of 1.5 and comparison with 1.3 and 1.7 solidity stages.
Chicago
Osborn, W. M, D. C Urasek, and R. D Moore. 1973. “Performance of a Single-Stage Transonic Compressor with a Blade-Tip Solidity of 1.5 and Comparison with 1.3 and 1.7 Solidity Stages,” 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.19740002621&authtype=sso&custid=ns315887.