Normal view MARC view ISBD view

FREE-FLIGHT HEAT-TRANSFER INVESTIGATION AT SUPERSONIC SPEEDS OF TWO SLENDER CONE-CYLINDER BODIES AT AN ANGLE OF ATTACK OF 8(DEGREE) WITH ONE BODY ROTATING

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1959Description: 41.DDC classification: NASA | MEMO 12-31-58L -

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 12-31-58L - (Browse shelf)	Not for loan		TR7754

Total holds: 0

Previous								Next
Previous	NASA MEMO 12-27-58L - WATER-FILM COOLING OF AN 80(DEGREE) TOTAL-ANGLE CONE AT A MACH NUMBER OF 2 FOR AIRSTREAM TOTAL TEMPERATURES UP TO 3,000(DEGREE)R	NASA MEMO 12-28-58L - BASIC PRESSURE MEASUREMENTS AT TRANSONIC SPEEDS ON A THIN 45(DEGREE) SWEPTBACK HIGHLY TAPERED WING WITH SYSTEMATIC SPANWISE TWIST VARIATIONS	NASA MEMO 12-30-58L - WEIGHT COMPARISON OF SEVERAL ATTITUDE CONTROLS FOR SATELLITES	NASA MEMO 12-31-58L - FREE-FLIGHT HEAT-TRANSFER INVESTIGATION AT SUPERSONIC SPEEDS OF TWO SLENDER CONE-CYLINDER BODIES AT AN ANGLE OF ATTACK OF 8(DEGREE) WITH ONE BODY ROTATING	NASA MEMO 12-3-58L - ANALYSIS OF FLIGHT-TEST MEASUREMENTS OF THE WING STRUCTURAL DEFORMATIONS IN ROUGH AIR OF A LARGE FLEXIBLE SWEPT-WING AIRPLANE	NASA MEMO 12-3-58W HEAT TRANSFER IN THE TURBULENT INCOMPRESSIBLE BOUNDRY LAYER III- ARBITRARY WALL TEMPERATURE AND HEAT FLUX.	NASA MEMO 1-23-59A - LOW-SPEED WIND-TUNNEL INVESTIGATION OF BLOWING BOUNDARY-LAYER CONTROL ON LEADING-AND TRAILING-EDGE FLAPS OF A LARGE-SCALE, LOW-ASPECT-RATIO, 45(DEGREE)SWEPT-WING AIRPLANE CONFIGURATION	Next

Bound With Nasa Memo 12-1-58l-12-31-58l

There are no comments for this item.

PKK Library