Home / Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 to 58 and Mach numbers from 0.6 to 2.
  • Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 to 58 and Mach numbers from 0.6 to 2.
  • Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 to 58 and Mach numbers from 0.6 to 2.
  • Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 to 58 and Mach numbers from 0.6 to 2.
  • Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 to 58 and Mach numbers from 0.6 to 2.
  • Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 to 58 and Mach numbers from 0.6 to 2.

Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 to 58 and Mach numbers from 0.6 to 2.

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    Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 to 58 and Mach numbers from 0.6 to 2.
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