Normal view MARC view ISBD view

Lee surface heating and flow phenomena on shuttle orbiters at large angles of attack and hypersonic speeds

Material type: materialTypeLabel

BookPublisher: Washington, D. C. National Aeronautics and Space Administration 1972Description: 42p.Subject(s): Hypersonic speeds

average rating: 0.0 (0 votes)

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Reference	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		TR12260

Total holds: 0

Previous								Next
Previous	Apollo experience report spacecraft heating environment and thermal protection for a launch through the atmosphere of the earth	Apollo experience report evolution of the attitude time line	Wind tunnel measurements of surface pressure fluctuations at mach numbers of 1.6, 2.0 and 2.5 using 12 different trasducers	Lee surface heating and flow phenomena on shuttle orbiters at large angles of attack and hypersonic speeds	NASA Technical Note [NASA TN D-4442]: Experimental investigation of acoustic liners to suppress screech in storable propellant rocket motors	NASA Technical Note [NASA TN D-4443]: Local afterbody heat transfer to a blunt two-dimensional configuration at mach 8	NASA Technical Note [NASA TN D-4444]: Texture strengthening and fracture toughness of titanium alloy sheet at room and cryogenic temperatures	Next

There are no comments for this item.

PKK Library