Transonic wind-tunnel investigation of the fin loads of a 1/8-scale model simulating the first stage of the Scout research vehicle

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086	0	⊔	‡aNAS 1.14:D-918
090	⊔	⊔	‡aTL521 ‡b.A3525 no. 918
100	1	⊔	‡aKelly, Thomas C.
245	1	0	‡aTransonic wind-tunnel investigation of the fin loads of a 1/8-scale model simulating the first stage of the Scout research vehicle / ‡cby Thomas C. Kelly.
260	⊔	⊔	‡aWashington : ‡bNational Aeronautics and Space Administration, ‡c[1961]
300	⊔	⊔	‡a28 p. : ‡bill. ; ‡c26 cm.
490	⊔	0	‡aNASA technical note, ‡x0499-9339 ; ‡vD-918
500	⊔	⊔	‡aPrepared at Langley Research Center.
500	⊔	⊔	‡a"June 1961."
500	⊔	⊔	‡aCover title.
504	⊔	⊔	‡aIncludes bibliographical references (p. 6).
538	⊔	⊔	‡aMode of access: Internet.
650	⊔	0	‡aAngle of attack (Aerodynamics)
650	⊔	0	‡aAerodynamic load.
650	⊔	0	‡aRockets (Aeronautics) ‡xFins ‡xTesting.
710	2	⊔	‡aLangley Research Center.
CID	⊔	⊔	‡a011443015
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DAT	1	⊔	‡a20141112165512.0 ‡b2025-01-02T19:11:31Z
DAT	2	⊔	‡a2025-01-02T18:30:02Z
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