Preisser, J. S., & Lowder, H. E. (1977). Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4. National Aeronautics and Space Administration.
Chicago Style (17th ed.) CitationPreisser, John S., and Harold E. Lowder. Comparison of Theoretical and Experimental Steady Wing Loads on a Space Shuttle Configuration at Mach Numbers of 0.6 and 1.4. Washington: National Aeronautics and Space Administration, 1977.
MLA (9th ed.) CitationPreisser, John S., and Harold E. Lowder. Comparison of Theoretical and Experimental Steady Wing Loads on a Space Shuttle Configuration at Mach Numbers of 0.6 and 1.4. National Aeronautics and Space Administration, 1977.
Warning: These citations may not always be 100% accurate.