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1.
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Maoism in India
: reincarnation of ultra-left wing extremism in the twenty-first century
by Chakrabarty, Bidyut | Kujur, Rajat Kumar. Material type:  Book; Format:
print
; Literary form:
not fiction
Description: xiv, 250p.Publisher: London Routledge 2010Availability: Items available for loan: PK Kelkar Library, IIT Kanpur [Call number: 335.43450954 C349m] (1).
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2.
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NASA Technical Note: AERODYNAMIC CHARACTERISTICS OF A PARASOL-WING-BODY COMBINATION UTILIZING FAVORABLE LIFT INTERFERENCE AT MACH NUMBERS FROM 3.00 TO 4.63
by Morris, Odell A | Mack, Robert J. Material type: Book Description: 36p.Publisher: Washington, D.C. NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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3.
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NASA Technical Note: AUTOMATED PRELIMINARY DESIGN OF SIMPLIFIED WING STRUCTURES TO SATISFY STRENGTH AND FLUTTER REQUIREMENTS
by Stroud, W. Jefferson | Dexter, Cornelia B | Stein, Manuel. Material type: Book Description: 137p.Publisher: Washington, D.C. NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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4.
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NASA Technical Note [NASA TN D-5272]: An experimental and theoretical investigation of a symmetrical and a cambered delta wing configuration at mach numbers from 2.0 to 10.7
by Washington. National Aeronautics and Space Administration (NASA) | Nelms, Walter P | Carmichael, Ralph L | Castellano, Charles R. Material type: Book Description: 31p.Publisher: Washington NASA 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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5.
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NASA Technical Note [NASA TN D-4322]: Static and dynamic longitudinal stability derivatives of a powered 0.18-scale model of a fan-in-wing VTOL aircraft
by Washington. National Aeronautics and Space Administration (NASA) | Chambers, Joseph R | Grafton, Sue B. Material type: Book Description: 64p.Publisher: Washington NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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6.
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NASA Technical Note [NASA TN D-4329]: Measurements of ground effect on a low-aspect-ratio ogee-wing airplane model and calculations of landing-flare trajectories
by Washington. National Aeronautics and Space Administration (NASA) | Lockwood, Vernard E | Phillips, W. Pelham. Material type: Book Description: 38p.Publisher: Washington NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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7.
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ANALYSIS OF WING SLIPSTREAM FLOW INTRACTION [NASA CR-1632]
by Jameson, Antony. Material type: Book; Format:
print
; Literary form:
not fiction
Description: iv, 145p.Publisher: Washington, D.C. NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA CR-1632 ] (1).
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8.
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NASA Technical Note: INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A HYPERSONIC TRANSPORT MODEL AT MACH NUMBERS TO 6
by Ellison, James C. Material type: Book Description: 79p.Publisher: Washington, D.C. NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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9.
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NASA Technical Note [NASA TN D-1946]: Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle
by Washington. National Aeronautics and Space Administration (NASA) | Johnson, Joseph L | Hassell, James L. Material type: Book Description: 72p.Publisher: Washington NASA 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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10.
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WIND-TUNNEL INVESTIGATION OF THE EFFECTS OF WING BODIES, FENCES, FLAPS AND A FUSELAGE ADDITION ON THE WING BUFFET RESPONSE OF A TRANSONIC TRANSPORT MODEL [NASA TN D-637]
by Cornette, Elden S. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 65p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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11.
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NASA Memorandum [NASA MEMO 4-27-59A]: Lift-drag ratios for an arrow wing with bodies at mach number 3
by Washington. National Aeronautics and Space Administration (NASA) | Jorgensen, Leland H. Material type: Book Description: 32p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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12.
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Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a mach number of 2.01 [NASA TN D-839]
by Spearman, M. Leroy. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 40p.Publisher: Washington, D.C. Nasa 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-839] (1).
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13.
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Investigation of a semispan tilting prpeller congiguration and effects of ratio of wing chord to propeller diameter on several smal-chord tilting-wing configurations [NASA TN D-1815]
by Spremann, Kenneth P. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 31p.Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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14.
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Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles
by Reed, Wilmer H | NASA Washington. Material type: Book; Format:
print
; Literary form:
not fiction
Description: various pagings.Publisher: Washington NASA 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D 1821-1830] (1).
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15.
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Effect of body cross section and width-height ratio on performance of bodies and delta-win-body combinations at mach 6.9 [NASA TN D-2886]
by Whitehead, Allen H. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 25p.Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2886] (1).
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16.
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Simulation of flight test conditions in the langley pilot transonic cryogenic tunnel [NASA TN D 7811-7820
by NASA : National Aeronautics and Space Administration. Material type: Book; Format:
print
; Literary form:
not fiction
Description: various pagings.Publisher: Washington NASA 1974Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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17.
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Transonic aerodynamics loading of awing-body-tial combination having A 52 degree centigradesweotback wing of aspect ratio 3 with conical wing chanber and body indentation for a design march number of 2 [NASA TN D-971]
by Cassetti, Malow D | Re, Richard J | Loge, William B. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 97p.Publisher: Washingto, D.C. NASA 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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18.
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A transonic investigation of changing indentation design mach number on the aerodynamic charecteristics of A 45degree sweptback-wing-body combination designed for high performance [NASA TN D-941]
by Loving, Donald L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 86p.Publisher: Washington, D. C. NASA 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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19.
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Rapid-transition tests of A 1/4-scale model of the till t wing aircraft [NASA TN D-946]
by Tosti, Louis P. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 72p.Publisher: Wahingtion, D. C. NASA NASAAvailability: No items available
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20.
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Rapid-transition tests of A 1/4-scale model of the till t wing aircraft [NASA TN D-946]
by Tosti, Louis P. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 72p.Publisher: Wahingtion, D. C. NASA NASAAvailability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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