Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.

Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.

$11.57
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Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
  • Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.
Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.

Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.

$11.57

Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / Leland H. Jorgensen and Edgar R.

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