Normal view MARC view ISBD view

INTERFERENCE HEATING FROM INTERACTIONS OF SHOCK WAVES WITH TURBULENT BOUNDARY LAYERS AT MACH 6

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1974Description: 71.DDC classification: NASA | TN D-7649

average rating: 0.0 (0 votes)

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-7649 (Browse shelf)	Not for loan		TR11639

Total holds: 0

Previous								Next
Previous	NASA TN D-7644 AN EVALUATION OF CONTRACTOR PROJECTED AND ACTUAL COSTS.	NASA TN D-7646 RELIABILITY-BASED ECONOMETRICS OF AEROSPACE STRUCTURAL SYSTEMS DESIGN CRITERIA AND TEST OPTIONS.	NASA TN D-7647 PARAMETER ESTIMATION TECHNIQUES AND APPLICATIONS IN AIRCRAFT FLIGHT TESTING.	NASA TN D-7649 INTERFERENCE HEATING FROM INTERACTIONS OF SHOCK WAVES WITH TURBULENT BOUNDARY LAYERS AT MACH 6	NASA TN D-765 EXPERIMENTAL HEAT TRANSFER AND PRESSURE DROP OF LIQUID HYDROGEN FLOWING THROUGH A HEATED TUBE	NASA TN D-7650 AERODYNAMIC AND FLOW-VISUALIZATION STUDIES OF VARIATIONS IN THE GEOMETRY OF IRREGULAR PLANFORM WINGS AT A MACH NUMBER OF 20.3.	NASA TN D-7651 THEORETICAL AND EXPERIMENTAL LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF AN ASPECT RATIO 0.25 SHARP-EDGE DELTA WING AT SUBSONIC, SUPERSONIC,AND HYPERSONIC SPEEDS	Next

Bound With Nasa Tn D-7648,7650-60

There are no comments for this item.

PKK Library