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FLIGHT INVESTIGATION TO DETERMINE THE LATERAL OSCILLATORY DAMPING ACCEPTABLE FOR AN AIRPLANE IN THE LANDING APPROACH

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BookSeries: NASA Memo. 12-10-58A.Publisher: Nasa, Washington, D.C. 1959Description: 33p.

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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-12-10-58A	Not for loan		TR8789

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Previous	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	BOUNDARY-LAYER TRANSITION MEASUREMENTS ON HEMISPHEREE OF VARIOUS SURFACE ROUGHNESSES IN A WIND TUNNEL AT MACH NUMBERS FROM 2.48 TO 3.55	EVALUTION OF SOME CONTROL-VOLUME TECHNIQUES FOR ANALYSIS OF SHOCK-BOUNDARY-LAYER INTERACTIONS IN SUPERSONIC INLETS	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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