Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0
Language: en
Pages: 110
Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0
Language: en
Pages: 100
Induced Side Forces on Bodies of Revolution at High Angle of Attack
Language: en
Pages: 52
Authors: Wardlaw, Jr. (Andrew B.)
Categories: Aerodynamic load
Type: BOOK - Published: 1975 - Publisher:

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Linear regression techniques are used to establish a quantitative description of side forces on bodies at high incidence. A data base is assembled concerning th