A Method For The Calculation Of External Lift Moment And Pressure Drag Of Slender Open Nose Bodies Of Revolution At Supersonic Speeds
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NACA Wartime Reports. Series L.
Author | : Clinton E. Brown |
Publisher | : |
Total Pages | : 20 |
Release | : 1946 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
An approximate method is presented for the calculation of the external lift, moment, and pressure drag of slender open-nose bodies of revolution of supersonic speeds. The lift, moment, and pressure drag of a typical ram-jet body shape are calculated at Mach numbers 1.45, 1.60, 1.75, and 3.00; and the lift and moment results are compared with available experimental data. The agreement of the calculated lift and moment data with the experimental data is excellent. The pressure-drag comparison was not presented because of the uncertainty of the amount of skin-friction drag present in the experimental results.
Wartime Report
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 284 |
Release | : |
Genre | : Aeronautics |
ISBN | : |
Index of NACA Technical Publications
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1370 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
NACA Wartime Report
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 712 |
Release | : 1945 |
Genre | : Aeronautics |
ISBN | : |
Report - National Advisory Committee for Aeronautics
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 752 |
Release | : 1945 |
Genre | : Aeronautics |
ISBN | : |
Annual Report - National Advisory Committee for Aeronautics
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : |
Release | : 1955 |
Genre | : Aeronautics |
ISBN | : |
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.