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THE FLUORESCENT-OIL FILM METHOD AND OTHER TECHNIQUES FOR BOUNDARY-LAYER FLOW VISUALIZATION

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BookPublisher: Nasa, Washington, D.C. 1959Description: 37.DDC classification: NASA | MEMO 3-17-59L

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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 MEMO 3-17-59L (Browse shelf)	Not for loan		TR7398

Total holds: 0

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Previous	NASA MEMO 3-12-59L THE EFFECT OF LIFT-DRAG RATIO AND SPEED ON THE ABILITY TO POSITION A GLIDING AIRCRAFT FOR A LANDING ON A 5,000-FOOT RUNWAY.	NASA MEMO 3-15-59L RESULTS OF A CYCLIC LOAD TEST OF AN RB-47E AIRPLANE COORD.NO.AF-AM-171	NASA MEMO 3-16-59W EFFECT OF CASCADE PARAMETERS ON ROTATING STALL	NASA MEMO 3-17-59L THE FLUORESCENT-OIL FILM METHOD AND OTHER TECHNIQUES FOR BOUNDARY-LAYER FLOW VISUALIZATION	NASA MEMO 3-2-59L WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 1.60 TO 4.50 OF THE STATIC-STABILITY CHARACTURISTICS OF TWO NONLIFTING VEHICLES SUITABLE FOR REENTRY	NASA MEMO 3-3-59E PERFORMANCE OF TWO BARON -MODIFIED S-816 ALLOYS IN A TURBOJET OPERATED AT 1650 DEGREE F	NASA MEMO 3-3-59L WIND-TUNNEL INVESTIGATION OF THE EFFECT OF ANGLE OF ATTACK AND FLAPPING-HINGE OFFSET ON PERIODIC BENDING MOMENTS AND FLAPPING OF A SMALL ROTOR	Next

Bound With Nasa Memo 3-2-59l - 3-16-59w Lack No. 9, 11, 13-14

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