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SUBSONIC WIND-TUNNEL INVESTIGATION OF A TWIN-ENGINE ATTACK AIRPLANE MODEL HAVING NONMETRIC POWERED NACELLES :

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BookPublisher: NASA, WASHINGTON, D.C. 1974Description: ,132.Subject(s): Literature -- Bibliography | Languages and languages -- BibliographyDDC classification: NASA TN D-7742

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-7742 (Browse shelf)	Not for loan		117216

Total holds: 0

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Previous	NASA TN D-7727 SOME ASPECTS OF OFTICAL FEEDBACK WITH CAMIUM SULFIDE AND RELATED PHOTOCONDUCTORS	NASA TN D-773 HOT-WIRE HEAT-LOSS CHARACTERISTICS AND ANEMOMETRY IN SUBSONIC CONTINUUM AND SLIP FLOW	NASA TN D-774 OPERATIONAL TECHNIQUE FOR TRANSITION OF SEVERAL TYPES OF V/STOL AIRCRAFT	NASA TN D-7742 SUBSONIC WIND-TUNNEL INVESTIGATION OF A TWIN-ENGINE ATTACK AIRPLANE MODEL HAVING NONMETRIC POWERED NACELLES	NASA TN D-7743 EXPERIMENTAL INVESTIGATION OF THE BRAKING AND CORNERING CHARACTERISTICS OF 30 X 11.5-14.5, TYPE VIII, AIRCRAFT TIRES WITH DIFFERENT TREAD PATTERNS	NASA TN D-7744 AN EXPERIMENTAL AND NUMERICAL STUDY OF WAVE MOTION AND UPSTREAM INFLUENCE IN A STRATIFIED FLUID	NASA TN D-7745 EFFECTS OF SIMULATED SOLAR RADIATION ON THE TRANSMISSION OF MAGNESIUM FLURIDE AND CRYOLITE THIN FILM	Next

Bound with NASA TN D-1743-1760 Lack No.1746,1748-1749,1752,1755,1758-1760

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