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LOW-SPEED LONGITUDINAL CHARACTERISTICS OF AN AIRPLANE CONFIGURATION INCLUDING EFFECTS OF CANARD AND WING TRAILING-EDGE FLAP CONTROLS IN COMBINATION

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BookPublisher: Nasa, Washington, D.C. 1959Description: 50.DDC classification: NASA | MEMO 4-22-59L

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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 4-22-59L (Browse shelf)	Not for loan		TR7401

Total holds: 0

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Previous	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	NASA MEMO 4-22-59L LOW-SPEED LONGITUDINAL CHARACTERISTICS OF AN AIRPLANE CONFIGURATION INCLUDING EFFECTS OF CANARD AND WING TRAILING-EDGE FLAP CONTROLS IN COMBINATION	NASA MEMO 4-23-59L ANALYTICAL INVESTIGATION OF A FLIKER-TYPE ROLL CONTROL FOR A MACH NUMBER 6 MISSILE WITH AERODYNAMIC CONTROLS OVER AN ALTITUDE RANGE OF 82,000 TO 282,000 FEET	NASA MEMO 4-2-59L - STABILITY CHARACTERISTICS FROM MACH NUMBER 1.0 TO 3.2 OF A MISSILE OF FINENESS RATIO 11.5 WITH A 10(DEGREE) FLARED-SKIRT AFTERBODY	NASA MEMO 4-27-59E - HEAT TRANSFER FROM CYLINDERS IN TRANSITION FROM SLIP FLOW TO FREE-MOLECULE FLOW	Next

Bound With Nasa Memo 4-20-59l-4-21-59l And 4-23-59l-4-30-59l Lack No.24and29

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