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8101.
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EXTENSION OF BOUNDARY-LAYER-SEPARATION CRITERIA TO A MACH NUMBER OF 6.5 BY UTILIZING FLAT PLATES WITH FORWARD-FACING STEPS
by Sterrett,James R | Emery,James C. Material type:  Book Description: 52.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-618 -] (1).
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8102.
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DETERMINATION OF THE REQUIRED NUMBER OF RANDOMLY SPACED COMMUNICATION SATELLITES
by Bennett,Floyd V, Coleman,Thomas L | Houbolt,John C. Material type: Book Description: 29.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-619 -] (1).
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8103.
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PILOTED SIMULATOR STUDY OF TAKEOFF PERFORMANCE AND HANDLING QUALITIES OF A DOUBLE-DELTA SUPERSONIC TRANSPORT
by Snyder,C Thomas | Jackson,Jr,Charles T. Material type: Book Description: 46.Publisher: Nasa, Washington, D.C. 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4396 -] (1).
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8104.
|
CHARACTERISTICS OF SOME SLENDER CAMBERED GOTHIC WINGS AT MACH NUMBERS FROM 0.4 TO 2.0
by Squire,L C. Material type: Book Description: 47.Publisher: Her Majesty'S Stationery Office, London 1962Availability: No items available Damaged (1).
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8105.
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PRESSURE DISTRIBUTIONS AND FLOW PATTERNS AT M=4.0 ON SOME DELTA WINGS
by Squire,L C. Material type: Book Description: 32,pts.2.Publisher: Her Majesty'S Stationery Office, London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3373 -] (1).
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8106.
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NON-LINEAR THEORY OF STEADY FORCES ON WINGS WITH LEADING-EDGE FLOW SEPARATION
by Garner,H C | Lehrian,Doris E. Material type: Book Description: 67.Publisher: Her Majesty'S Stationery Office, London 1963Availability: No items available Damaged (1).
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8107.
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MEASUREMENTS OF THE DIRECT OSCILLATORY DERIVATIVES FOR A LINEAR BENDING MODE ON FOUR RIGID HALF-SPAN MODELS AT SUBSONIC AND TRANSONIC SPEEDS, IN CLOSED AND SLOTTED TUNNELS
by Wight,K C | Nixon,J A. Material type: Book Description: 20.Publisher: Her Majesty'S Stationery Office, London 1963Availability: No items available Damaged (1).
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8108.
|
SOME TESTS ON HIGH-REACTION COMPRESSOR BLADING
by Turner,R C | Burrows,R A. Material type: Book Description: 19.Publisher: Her Majesty'S Stationery Office, London 1963Availability: No items available Damaged (1).
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8109.
|
CONCEPT OF A MANNED SATELLITE REENTRY WHICH IS COMMPLETED WITH A GLIDE LANDING
by Donald C Cheatham. Material type: Book Description: 44.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-226 -] (1).
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8110.
|
HIGH-ALTITUDE PERFORMANCE OF A 64-FOOT-DIAMETER RING SAIL PARACHUTE
by Kurbjun,Max C. Material type: Book Description: 14.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-232 -] (1).
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8111.
|
PROGRESS IN SUPERRALLOYS
by Freche,John C. Material type: Book Description: 13.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2495 -] (1).
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8112.
|
REAL-GAS INVISCID NOZZLE CONTOURS FOR NITROGEN AT MACH 15, 17, AND 19 WITH TABULATED PROPERTIES FOR THE CALCULATION OF BOUNDARY-LAYER EFFECTS
by Johnson,Charles B | Ellison,James C. Material type: Book Description: 124.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2496 -] (1).
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8113.
|
DYNAMIC MODEL INVESTIGATION OF THE LANDING CHARACTERISTICS OF A MANNED SPACECRAFT
by Thompson,William C. Material type: Book Description: 33.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2497 -] (1).
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8114.
|
WIND TUNNEL TEST OF A FULL-SCALE, 1.1 PRESSURE RATIO, DUCTED LIFT-CRUISE FAN
by Giulianetti,Demo J, Biggers,James C | Corsiglia,Victor R. Material type: Book Description: 45.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2498 -] (1).
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8115.
|
HIGHLY LOADED MULTI-STAGE FAN DRIVE TURBINE - LEANED STATOR CONFIGURATION DESIGN
by Evans,D C | Wolfmeyer,G W. Material type: Book Description: vii,30.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA CR-2096 -] (1).
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8116.
|
HIGHLY LOADED MULTI-STAGE FAN DRIVE TURBINE-TANDEM BLADE CONFIGURATION DESIGN
by Evans,D C | Wolfmeyer,G W. Material type: Book Description: viii,59.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA CR-2097 -] (1).
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8117.
|
NASA Technical Note [NASA TN D-5934]: A pplication of Brouwer's artificial-satellite theory to computation of the state transition matrix
by Washington. National Aeronautics and Space Administration (NASA) | Born, George H | Kirkpatrick, James C. Material type: Book Description: 35p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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8118.
|
EXPERIMENTAL STUDY OF ONE-AND TWO-COMPONENT LOW TURBULENCE CONFINED COAXIAL FLOWS
by Bennett,John C | Johnson,Bruce V. Material type: Book Description: 87.Publisher: Nasa, Washington, D.C. 1971Availability: No items available Damaged (1).
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8119.
|
DEVELOPMENT OF A ELECTROLYTE CARBON DIOXIDE AND WATER REDUCTION SYSTEM FOR OXYGEN RECOVERY
by Elikan,L, Morris,J P | Wu,C K. Material type: Book Description: xiii,169.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA CR-2014 -] (1).
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8120.
|
FLIGHT TESTING TECHNIQUES FOR THE EVALUATION OF LIGHT AIRCRAFT STABILITY DERIVATIVES - A REVIEW AND ANALYSIS
by Smetana,Frederick O, Summey,Delbert C | Johnson,W Donald. Material type: Book Description: iii,110.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA CR-2016 -] (1).
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