Normal view MARC view ISBD view

EVALUTION OF SOME CONTROL-VOLUME TECHNIQUES FOR ANALYSIS OF SHOCK-BOUNDARY-LAYER INTERACTIONS IN SUPERSONIC INLETS

Material type: materialTypeLabel

BookSeries: NASA Technical Memorandum. Publisher: NASA, Washington, D.C. 1975Description: 183p.Subject(s): Aerodynamics

average rating: 0.0 (0 votes)

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 TM X-3186	Not for loan		TR10281

Total holds: 0

Previous								Next
Previous	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	CONDUCTIVITIES OF THE IONIC COMPLEXES OF TWO CYCLIC POLETHERS	IRRADIATION AND MEASUREMENTS OF FLUORINATED ETHYLENE-PROPYLENE-A ON SILICON SOLAR CELLS IN VACUUM	COLD-AIR STUDY OF THE EFFECT ON TURBINE STATOR BLADE AERODYNAMIC PERFORMANCE OF COOLANT EJECTION FROM VARIOUS TRAILING-EDGE SLOT GEOMETRIES	Next

Technical Memorandum X-3181-90
Bound Vol. No.TR117214; contents:TR10277-10286

There are no comments for this item.

PKK Library