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EFFECT OF WING ASPECT RATIO AND FLAP SPAN ON AERODYNAMIC CHARACTERISTICS OF AN EXTERNALLY BLOWN JET-FLAP STOL MODEL

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BookPublisher: Nasa, Washington, D.C. 1973Description: 136.DDC classification: NASA | TN D-7205

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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 TN D-7205 (Browse shelf)	Not for loan		TR14762

Total holds: 0

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Previous	NASA TN D-7202 FLIGHT-MEASURED BASE PRESSURE COEFFICIENTS FOR THICK BOUNDARY-LAYER FLOW OVER AN AFT-FACING STEP FOR MACH NUMBERS FROM 0.4 TO 2.5	NASA TN D-7203 EXPERIMENTAL INVESTIGATION OF THE CORNERING CHARACTERISTICS OF A C40 X 14-21 CANTILEVER AIRCRAFT TIRE	NASA TN D-7204 DESIGN AND EVALUATION OF AN OPTICAL FINE-POINTING CONTROL SYSTEM FOR TELESCOPES UTILIZING A DIGITAL STAR SENSOR	NASA TN D-7205 EFFECT OF WING ASPECT RATIO AND FLAP SPAN ON AERODYNAMIC CHARACTERISTICS OF AN EXTERNALLY BLOWN JET-FLAP STOL MODEL	NASA TN D-7206 FRICTION, WEAR, AND TRANSFER OF CARBON AND GRAPHITE TO COPPER, CHROMIUM, AND ALUMINUM METAL SURFACES IN VACUUM	NASA TN D-7207 COOLANT-SIDE HEAT-TRANSFER RATES FOR A HYDROGEN-OXYGEN ROCKET AND A NEW TECHNIQUE FOR DATA CORRELATION	NASA TN D-7208 THEORY OF DISORDERED HEISENBERG FERROMAGNETS	Next

Bound With Nasatn D-7200-7204,7206-7210

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