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WIND-TUNNEL INVESTIGATION OF SUBSONIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A TILTABLE-WING VERTICAL-TAKE-OFF-AND-LANDING SUPERSONIC BOMBER CONFIGURATION INCLUDING TURBOJET POWER EFFECTS

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BookPublisher: Nasa, Washington, D.C. 1959Description: 89.DDC classification: NASA | MEMO 1-8-59L -

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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 1-8-59L - (Browse shelf)	Not for loan		TR7664

Total holds: 0

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Previous	NASA MEMO 1-5-59L - EFFECT OF BEAM LOADING ON WATER IMPACT LOADS AND MOTIONS	NASA MEMO 1-6-59L - INVESTIGATION OF SPHERICAL-WAVE-INITIATED FLOW FIELDS AROUND BODIES	NASA MEMO 1-7-59L - WIND-TUNNEEL INVESTIGATION OF ROTOR BEHAVIOR UNDER EXTREME OPERATING CONDITIONS WITH A DESCRIPTION OF BLADE OSCILLATIONS ATTRIBUTED TO PITCH-LAG COUPLING	NASA MEMO 1-8-59L - WIND-TUNNEL INVESTIGATION OF SUBSONIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A TILTABLE-WING VERTICAL-TAKE-OFF-AND-LANDING SUPERSONIC BOMBER CONFIGURATION INCLUDING TURBOJET POWER EFFECTS	NASA MEMO 1-9-59L - HYDRODYNAMIC IMPACT-LOAD ALLEVIATION WITH A PENETRATING HYDRO-SKI	NASA MEMO 2-11-59E EFFECT OF STATOR AND ROTOR ASPECT RATIO ON TRANSONIC-TURBINE PERFORMANCE	NASA MEMO 2-12-59A - EFFECTS OF TARGET AND MISSILE CHARACTERISTICS ON THEORETICAL MINIMUM MISS DISTANCE FOR A BEAM-RIDER GUIDANCE SYSTEM IN THE PRESENCE OF NOISE	Next

Bound With Nasa Memo 1-2-59l-1-10-59l

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