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LARGE-SCALE WIND-TUNNEL TESTS OF AN AIRPLANE MODEL WITH AN UNSWEPT,ASPECT-RATIO-10 WING,TWO PROPELLERS,AND BLOWING FLAPS

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BookSeries: NASA Memorandum. 12-3-58A.Publisher: Nasa, Washington, D.C. 1958Description: 47p.Subject(s): AerospaceDDC classification: NASA

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA MEMO 12-3-58A	Not for loan		TR8787

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Previous	NASA Technical Note [NASA TN D-5939]: An adaptive controller for space base spin plane orientation	NASA Technical Note : STABILITY AND CONTROL CHARACTERISTICS OF A 0.0667-SCALE MODEL OF THE FINAL VERSION OF THE NORTH AMERICAN X-15 RESEARCH AIRPLANE (CONFIGURATION 3) AT TRANSONIC SPEEDS	NASA Technical Memorandum: METEOROID HAZARD TO SPACE VEHICLES IN ORBIT NEAR THE EARTH	LARGE-SCALE WIND-TUNNEL TESTS OF AN AIRPLANE MODEL WITH AN UNSWEPT,ASPECT-RATIO-10 WING,TWO PROPELLERS,AND BLOWING FLAPS	THREE-DIMENSIONAL ORBITS OF EARTH SATELLITES,INCLUDING EFFECTS OF EARTH OBLATENESS AND ATMOSPHERIC ROTATION	FLIGHT INVESTIGATION TO DETERMINE THE LATERAL OSCILLATORY DAMPING ACCEPTABLE FOR AN AIRPLANE IN THE LANDING APPROACH	SUBSONIC AERODYNAMIC CHARACTERISTICS OF SEVERAL BLUNT,LIFTING,ATMOSPHERIC-ENTRY SHAPES	Next

NASA Memorandum 12-1-58A-12-4-58A; 12-24-58A-12-31-58A
Bound Vol. No.102443;Contents: TR8786-95

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