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BASIC PRESSURE MESUREMENTS AT TRANSONIC SPEEDS ON A THIN 45 DEGREE CELSIUS SWEPTBACK HIGHLY TAPERED WING WITH SYSTEMATIC SPANWISE TWIST VARIATION

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BookPublisher: Nasa, Washington, D.C. 1959DDC classification: NASA | MEMO 5-12-59L

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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 5-12-59L (Browse shelf)	Not for loan Untraceable		TR7404

Total holds: 0

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Previous	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	NASA MEMO 5-18-59A THE EFFECTS OF STREAMWISE-DEFLECTED WING TIPS ON THE AERODYNAMIC CHARACTERISTICS OF AN ASPECT-RATIO-2 TRIANGULAR WING, BODY, AND TAIL COMBINATION	Next

Bound With Nasa Memo 5-13-59l-5-28-59l Lack No.14-17, 19, 21-22, 27

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