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TRANSONIC AERODYNAMIC CHARACTURISTICS OF A 45DEGREE SWEPT-WING-FUSELAGE MODEL WITH A FINNED AND UNFINNED BODY PYLON-MOUNTED BENEATH THE FUSELAGE OR WING, INCLUDING MEASUREMENTS OF BODY LOADS

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BookPublisher: Nasa, Washington, D.C. 1959Description: 57.DDC classification: NASA | MEMO 4-20-59L

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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 4-20-59L (Browse shelf)	Not for loan Untraceable		TR7399

Total holds: 0

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Previous	NASA MEMO 4-15-59L - CHARTS OF THE INDUCED VELOCITIES NEAR A LIFTING ROTOR	NASA MEMO 4-17-59L - AIRPLANE MEASUREMENTS OF ATMOSPHERIC TURBULENCE AT ALTITUDES BETWEEN 20,000 AND 55,000 FEET FOR FOUR GEOGRAPHIC AREAS	NASA MEMO 4-19-59L - Flight performance of a transonic turbine-driven propeller designed for minimum noise	NASA MEMO 4-20-59L TRANSONIC AERODYNAMIC CHARACTURISTICS OF A 45DEGREE SWEPT-WING-FUSELAGE MODEL WITH A FINNED AND UNFINNED BODY PYLON-MOUNTED BENEATH THE FUSELAGE OR WING, INCLUDING MEASUREMENTS OF BODY LOADS	NASA MEMO 4-21-59E - ANALYSIS OF FLOW-SYSTEM STARTING DYNAMICS OF TURBOPUMP-FED LIQUID-PROPELLANT ROCKET	NASA MEMO 4-21-59L INVESIGATION OF THE CHAACTERISTICS OF AN ACCELERATION-TYPE TAKE-OFF INDICATOR IN A LARGE JET AIRPLANE	NASA MEMO 4-22-59E - PRELIMINARY ANALYSIS OF THE EFFECT OF FLOW SEPARATION DUE TO ROCKET JET PLUMING ON AIRCRAFT DYNAMIC STABILITY DURING ATMOSPHERIC EXIT	Next

Bound With Nasa Memo 4-20-59l-4-30-59l Lack No.24-29

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