Limited space available for stowage of missiles aboard aircraft led to consideration of folded wing surfaces; method for computing aerodynamic loads on slender missiles with complicated cross-sections is applied to predict loads for missiles with folding wings; comparison of calculations with wind tunnel measurements indicates that method provides satisfactory first estimates of aerodynamic properties of such missiles.
Characteristics of slender wing-body combinations with folding wings
Aircraft Eng
Aircraft Engineering ; 31 , n 359
1959
8 pages
Aufsatz (Zeitschrift)
Englisch
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Characteristics of Slender Wing-Body Combinations with Folding Wings
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