Normal view MARC view ISBD view

THE INTERACTION OF AN OBLIQUE SHOCK WAVE WITH ALAMINAR BOUNDARY LAYER

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1959Description: 49.DDC classification: NASA | MEMO 2-18-59W -

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 MEMO 2-18-59W - (Browse shelf)	Not for loan Untraceable		TR7732

Total holds: 0

Previous								Next
Previous	NASA MEMO 2-17-59E EFFECTS OF EXTERNAL STREAM ON THE PERFORMANCE OF ISENTROPIC PLUG-TYPE NOZZLES AT MACH NUMBERS OF 2.0,1.8 AND 1.5	NASA MEMO 2-17-59L - SOME EFFECTS OF YAW DAMPING ON AIRPLANE MOTIONS AND VERTICAL-TAIL LOADS IN TURBULENT AIR	NASA MEMO 2-18-59L - EVALUATION OF SEVERAL APPOXIMATE METHODS FOR CALCULATING THE SYMMETRICAL BENDING-MOMENT RESPONSE OF FLEXIBLE AIRPLANES TO ISOTROPIC ATMOSPHERIC TURBULENCE	NASA MEMO 2-18-59W - THE INTERACTION OF AN OBLIQUE SHOCK WAVE WITH ALAMINAR BOUNDARY LAYER	NASA MEMO 2-19-59A - EXPERIMENTAL INVESTIGATION OF CIRCULAR INTERNAL-COMPRESSION INLETS WITH TRANSLATING CENTERBODIES EMPLOYING BOUNDARY-LAYER REMOVAL AT MACH NUMBERS FROM 0.85 TO 3.50	NASA MEMO 2-19-59L - FLIGHT INVESTIGATION OF AN AUTOMATIC THROTTLE CONTROL IN LANDING APPROACHES	NASA MEMO 2-20-59A - FULL-SCALE WIND-TUNNEL INVESTIGATION OF A JET FLAP IN CONJUNCTION WITH A PLAIN FLAP WITH BLOWING BOUNDARY-LAYER CONTROL ON A 35(DEGREE) SWEPTBACK-WING AIRPLANE	Next

Bond With Nasa Memo 2-5-59w-2-24-59w

There are no comments for this item.

PKK Library