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Art
J-GLOBAL ID:201602004766190807   Reference number:62A0061435

Aerodynamicderivative characteristics of the X research airplane as determined from flight testa for Mach numbers from to.

マッハ数範囲0,6~3.4の飛行試験で得られたX-15の空力微係数について
Author (3):
Material:
Volume: 1962  Issue: D-1060  Page: 1-68  Publication year: 1962
JST Material Number: B0433A  CODEN: NASCA   Document type: Reports
Article type: 原著論文  Country of issue: United States (USA) 
Terms in the title (4):
Terms in the title
Keywords automatically extracted from the title.

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