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1.
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REAL-TIME FLIGHT TEST DATA DISTRIBUTION AND DISPLAY
by Nesel,Michael C | Hammons,Kevin R. Material type:  Book; Format:
print
; Literary form:
not fiction
Publisher: Naca, Washington 1988Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: 629.13453 M582R] (1).
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2.
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Active controls
: a look at analytical methods and associated tools
by Newsom, J. R. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 13p.Publisher: Hampton Langley Research Center 1984Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: 629.1323 Ac85] (1).
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3.
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NASA TM [X-1110]
: USE OF A SINGLE TURNING VANE TO ELIMINATE FLOW SEPERATION IN A SPACE-LIMITED 90(DEGREE) INTAKE ELBOW OF AN AXIAL-FLOW COMPRESSOR
by Pinckney, S. Z. Description: 28p.Publisher: Washington National Aeronautics and Space Administration 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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4.
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NASA TM [X-1111]
: MECHANISM OF FORMATION OF CERTAIN METASTABLE PEAKS NOTED ON A CYCLOIDAL FOCUSING MASS SPECTROMETER
by Davies, Myron O. Description: 7p.Publisher: Washington National Aeronautics and Space Administration 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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5.
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NASA TM [X-1113]
: AN AUTOMATIC SYSTEM FOR DETERMINING SOLAR ABSORPTANCE AND THERMAL EMITTANCE OF SURFACES FROM SPECTRAL NORMAL REFLECTANCE MEASUREMENTS
by Teichman, Louis A | Burks, Harold D. Description: 11p.Publisher: Washington National Aeronautics and Space Administration 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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6.
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NASA TM [X-1119]
: INVESTIGATION OF ATLAS SOLID FUEL RETARDING ROCKET DURING ATLAS-CENTAUR SEPARATION TESTS
by Washington.National Aeronautics and Space Administration | Heath, Richard W | Synor, Henry | Schmiedlin, Ralph F | Povolny, John H. Description: 19p.Publisher: Washington National Aeronautics and Space Administration 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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7.
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NASA TM [X-1123]
: THE EXPLORER XXIII MICROMETEROID SATELLITE
by O'Neal, Robert L. Description: 56p.Publisher: Washington National Aeronautics and Space Administration 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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8.
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NASA TM [X-72]
: LOW-SPEED STATIC LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS OF A VARIABLE-INCIDENCE DELTA-WING CANARD MODEL WITH HIGH-LIFT CANARD SURFACES
by Cone, Clarence D. Description: 71.Publisher: Nasa,Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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9.
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NASA TM [X-75]
: EXPERIMENTAL AND ANALYTICAL STUDY OF ROLLING-VELOCITY AMPLIFICATION DURING THE THRUSTING PROCESS FOR TWO 10-INCH-DIAMETER SPHERICAL ROCKET MOTORS IN FREE FLIGHT
by Martz, C. William | Swain, Robert L. Description: 36.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-75 -] (1).
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10.
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NASA TM [X-83]
: OVERXPANDED PERFORMANCE OF 6 AND 9 WITH AND WITHOUT SUPERSONIC EXTERNAL FLOW
by Musial, Norman T | Ward,James J. Description: 25.Publisher: Nasa, Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-83 -] (1).
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11.
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NASA TM [X-85]
: CASCADE INVESTIGATION OF COOLING CHARACTERISTICS OF A CORRUGATED-INSERT AIR-COOLED TURBINE BLADE FOR USE IN A TURBOPROP ENGINE
by Richards, Hadley T. Description: 14.Publisher: Nasa, Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-85 -] (1).
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12.
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NASA TM [X-86]
: EXPERIMENTAL INVESTIGATION OF A 0.35 HUB-TIP RADIUS RATIO TRANSONIC AXIAL FLOW ROTOR DESIGNED FOR 40 POUNDS PER SECOND PER SQUARE FOOT WITH A DESIGN TIP DIFFUSION FACTOR OF 0.20
by Yasaki, Paul T | Montgomery, John C. Description: 37p.Publisher: Nasa, Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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13.
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NASA TM [X-786]
: MATERIALS PROBLEMS IN CHEMICAL LIQUID-PROPELLANT ROCKET SYSTEMS
by Gilbert, L. L. Description: 41.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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14.
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NASA TM [X-92]
: EFFECTS OF WING-CRANK, LEADING-EDGE EXTENSIONS AND HORIZONTAL-TALL HEIGHT ON THE LONGITUDINAL STABILITY OF SWEPT-WING MODELS AT MACH NUMBERS FROM 0.6 TO 1.4
by Wakefield, Roy M. Description: 116.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-92 -] (1).
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15.
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NASA TM [X-100]
: COMPARISON OF ROCKET PERFORMANCE USING EXHAUST DIFFUSER AND CONVENTIONAL TECHNIQUES FOR ALTITUDE SIMULATION
by Sivo, Joseph N | Peters, Daniel J. Description: 17p.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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16.
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INVESTIGATION OF A PHOTOGRAPHIC TECHNIQUE OF MEASURING HIGH SURFACE TEMPERATURES
by Siviter,James H | Strass,H. Kurt. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 15p.Publisher: NASA, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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17.
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EXPERIMENTAL INVESTIGATION OF COMPRESSOR STALL USING AN ON-LINE DISTORTION INDICATOR AND SIGNAL CONDITIONER
by Costakis,William G | Wenzel,Leon M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 31p.Publisher: NASA, Washington, D.C. 1975Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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18.
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AERODYNAMIC ANALYSIS OF SEVERAL HIGH THROAT MACH NUMBER INLETS FOR THE QUIET CLEAN SHORT-HAUL EXPERIMENTAL ENGINE
by Albers,James A | Hirn,John J | Stockman,Norbert O. Material type: Book Description: 19p.Publisher: NASA, Washington, D.C. 1975Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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19.
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DIGITAL COMPUTER STUDY OF NUCLEAR REACTOR THERMAL TRANSIENTS DURING STARTUP OF 60-K WE BRAYTON POWER CONVERSION SYSTEM
by Jefferies,Kent S | Tew,Roy C. Material type: Book Description: 18p.Publisher: NASA, Washington, D.C. 1974Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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20.
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WIND-TUNNEL INVESTIGATION OF HELICOPTER-ROTOR WAKE EFFECTS ON THREE HELICOPTER FUSELAGE MODELS
by Wilson,John C | Mineck,Raymond E. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 205p.Publisher: NASA, Washington, D.C. 1975Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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