Aerodynamic Characteristics Of Wraparound Fins Mounted On Bodies Of Revolution And Rheir Influence On The Missile Static Stability At Mach Numbers From 03 To 13
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Language: en
Pages: 0
Pages: 0
Type: BOOK - Published: 1972 - Publisher:
AMCDR-1001-Vol-1See also Volume 2, AD-772 670.*Guided missiles, *Fins, Tube launched, Aerodynamic forces, Pitch(Motion), Roll, Yaw, Angle of attackWraparound fi
Language: en
Pages: 376
Pages: 376
Type: BOOK - Published: 1972 - Publisher:
Experimental aerodynamic investigations were conducted for several wraparound fins and one planar fin configuration on bodies of revolution at Mach number rangi
Language: en
Pages: 0
Pages: 0
Type: BOOK - Published: 1972 - Publisher:
OL-2AMCDR-1001-Vol-2See also Volume 1, AD-772 669.*Guided missiles, *Fins, Tube launched, Aerodynamic forces, Pitch(Motion), Roll, Yaw, Angle of attackWraparoun
Language: en
Pages: 606
Pages: 606
Type: BOOK - Published: 1972 - Publisher:
Experimental aerodynamic investigations were conducted for several wraparound fins and one planar fin configuration on bodies of revolution at Mach number rangi
Language: en
Pages: 306
Pages: 306
Type: BOOK - Published: 1972 - Publisher:
Experimental aerodynamic investigations were conducted in the AEDC-4T wind tunnel for several wraparound fins with straight and with swept leading edge mounted