Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins From Mach 0.60 to 4.63

Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins From Mach 0.60 to 4.63

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Product Description

Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins From Mach 0.60 to 4.63

Technical Specifications

Country
USA
Brand
Bibliogov
Manufacturer
Bibliogov
Binding
Paperback
Height
9.69
Length
7.44
Weight
0.50044933474
Width
0.25
NumberOfItems
1
Author
Allen, Jerry M