Normal view MARC view ISBD view

SOME BASIC ASPECTS OF MAGNETOHYDRODYNAMIC BOUNDARY-LAYER FLOWS

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1959Description: 42.DDC classification: NASA | MEMO 4-9-59L -

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 4-9-59L - (Browse shelf)	Not for loan Untraceable		TR7690

Total holds: 0

Previous								Next
Previous	NASA MEMO 4-3-59L - FORMULAS PERTINENT TO THE CALCULATION OF FLOW-FIELD EFFECTS AT SUPERSONIC SPEEDS DUE TO WING THICKNESS	NASA MEMO 4-4-59L - EFFECTS OF FOREBODY DEFLECTION ON STABILITY AND CONTROL CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION WITH A HIGH TRAPEZOIDAL WING AT A MACH NUMBER OF 2.01	NASA MEMO 4-9-59E - EXPLORATORY INVESTIGATION OF AERODYNAMIC FLAMEHOLDERS FOR AFTERBURNER APPLICATION	NASA MEMO 4-9-59L - SOME BASIC ASPECTS OF MAGNETOHYDRODYNAMIC BOUNDARY-LAYER FLOWS	NASA MEMO 5-12-59L BASIC PRESSURE MESUREMENTS AT TRANSONIC SPEEDS ON A THIN 45 DEGREE CELSIUS SWEPTBACK HIGHLY TAPERED WING WITH SYSTEMATIC SPANWISE TWIST VARIATION	NASA MEMO 5-13-59L MEASUREMENTS OF TOTAL HEMISPHERICAL EMISSVTTY OF SEVERAL STABLY OXIDIZED NIKEL-TITANIUM CARBIDE CEMENTED HARD METALS FROM 600 D/F TO 1,600 D/F	NASA MEMO 5-16-59A THE STATIC AND DYNAMIC ROTARY STABILITY DERIVATIVES AT SUBSONIC SPEEDS ON AN AIRPLANE MODEL HAVING WING AND TAIL SURFACES SWEPT BACK 45	Next

Bound With Nasa Memo 4-1-59l-4-19-59l

There are no comments for this item.

PKK Library