cranfield0056

analysi applic hyperson similar law studi flow bodi revolut zero angl attack hyperson similar law deriv tsien investig compar pressur distribut along bodi revolut zero angl attack make comparison particular attent given determin limit mach number fine ratio similar law appli purpos investig pressur distribut determin method characterist ogiv cylind valu mach number fine ratio vari compar pressur variou cone cone cylind also compar studi pressur distribut present demonstr hyperson similar law applic wider rang valu mach number fine ratio might expect assumpt made deriv signific sinc within rang applic law singl pressur distribut exist similarli shape bodi ratio free stream mach number fine ratio constant chart present rapid determin pressur distribut ogiv cylind combin mach number fine ratio within defin limit