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SOME EFFECTS OF YAW DAMPING ON AIRPLANE MOTIONS AND VERTICAL-TAIL LOADS IN TURBULENT AIR

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BookPublisher: Nasa, Washington, D.C. 1959Description: 8.DDC classification: NASA | MEMO 2-17-59L -

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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 2-17-59L - (Browse shelf)	Not for loan		TR7538

Total holds: 0

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Previous	NASA MEMO 2-16-59L - EFFECT OF ADSORBED NITROGEN ON THE THERMIONIC EMISSION FROM LANTHANUM HEXABORIDE	NASA MEMO 2-17-59 - USE OF A STANTON TUBE FOR SKIN-FRICTION MEASUREMENTS	NASA MEMO 2-17-59E EFFECTS OF EXTERNAL STREAM ON THE PERFORMANCE OF ISENTROPIC PLUG-TYPE NOZZLES AT MACH NUMBERS OF 2.0,1.8 AND 1.5	NASA MEMO 2-17-59L - SOME EFFECTS OF YAW DAMPING ON AIRPLANE MOTIONS AND VERTICAL-TAIL LOADS IN TURBULENT AIR	NASA MEMO 2-18-59L - EVALUATION OF SEVERAL APPOXIMATE METHODS FOR CALCULATING THE SYMMETRICAL BENDING-MOMENT RESPONSE OF FLEXIBLE AIRPLANES TO ISOTROPIC ATMOSPHERIC TURBULENCE	NASA MEMO 2-18-59W - THE INTERACTION OF AN OBLIQUE SHOCK WAVE WITH ALAMINAR BOUNDARY LAYER	NASA MEMO 2-19-59A - EXPERIMENTAL INVESTIGATION OF CIRCULAR INTERNAL-COMPRESSION INLETS WITH TRANSLATING CENTERBODIES EMPLOYING BOUNDARY-LAYER REMOVAL AT MACH NUMBERS FROM 0.85 TO 3.50	Next

Bound With Nasa Memo 2-15-59l-2-28-59l

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