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21.
|
NASA Technical Note [NASA TN D-3027]: Illustration of design methods for power reduction in logical systems
by Washington. National Aeronautics and Space Administration (NASA) | Curtis, H. Allen. Material type:  Book Description: 19p.Publisher: Washington NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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22.
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NASA Technical Note [NASA TN D-6292]: Experimental investigation of the use of slotted test-section walls to reduce wall interference for high-lift-model testing
by Washington. National Aeronautics and Space Administration (NASA) | Grunwald, Kalman J. Material type: Book Description: 72p.Publisher: Washington NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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23.
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NASA Technical Note [NASA TN D-6117]: Utilization of a fixed-base simulator to study the stall and spin characteristics of fighter airplanes
by Washington. National Aeronautics and Space Administration (NASA) | Moore, Frederick L. Material type: Book Description: 34p.Publisher: Washington NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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24.
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NASA Technical Note [NASA TN D-5661]: Design charts of static and rotary stability derivatives for cropped double-delta wings in subsonic compressible flow
by Washington. National Aeronautics and Space Administration (NASA) | Lamar, John E. Material type: Book Description: 79p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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25.
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NASA Technical Note [NASA TN D-5662]: Effects of ground proximity on the longitudinal aerodynamic characteristics of an unswept aspect-ratio-10 wing
by Washington. National Aeronautics and Space Administration (NASA) | Carter, Arthur W. Material type: Book Description: 60p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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26.
|
NASA TN [D-6553]
: GENENG II- A PROGRAM FOR CALCULATING DESIGN AND OFF-DESIGN PERFORMANCE OF TWO-AND THREE-SPOOL TURBOFANS WITH AS MANY AS THREE NOZZIES
by Fishbach, Lanrence H | Koenig, Robert W. Description: 184p.Publisher: NASA, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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27.
|
NASA TN [D-6556]
: RESPONSE OF A RADIAL-BLADED CENTRIFUGAL PUMP TO SINUSOIDAL DISTURBANCES FOR NONCAVITATING FLOW
by Anderson, Douglas A | Blade, Robert J. Description: 51p.Publisher: NASA, Washington, D.C. 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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28.
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NASA Technical Note [NASA TN D-545]: A note on the drag due to lift of delta wings at mach numbers up to 2.0
by Washington. National Aeronautics and Space Administration (NASA) | Osborne, Robert S | Kelly, Thomas C. Material type: Book Description: 14p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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29.
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NASA Technical Note [NASA TN D-549]: Heat-transfer measurements at a mach number of 4.95 on two 60 [degree] swept delta wings with blunt leading edges and dihedral angles of 0 [degree] and 45 [degree]
by Washington. National Aeronautics and Space Administration (NASA) | Stainback, P. Calvin. Material type: Book Description: 50p.Publisher: Washington NASA 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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30.
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Effects of configutation modifications on aerodynamic charectristics of tension shell shapes at mach 3.0 [NASA TN D-4080]
by Sawyer, James Wayne | Deveikis, William D. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 37p.Publisher: Washington, D. C. National Aeronautics and Space Administration Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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31.
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NASA Technical Note [NASA TN D-383]: Theoretical calculations of the pressures forces, and moments due to various lateral motions acting on tapered sweptback vertical tails with supersonic leading and trailing edges
by Washington. National Aeronautics and Space Administration (NASA) | Margolis, Kenneth | Elliott, Miriam H. Material type: Book Description: 126p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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32.
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NASA Technical Note [NASA TN D-389]: The longitudinal aerodynamic characteristics of a sweptback wing-body combination with and without end plates at mach numbers from 0.40 to 0.93
by Washington. National Aeronautics and Space Administration (NASA) | Henderson, William P. Material type: Book Description: 22p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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33.
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NASA Technical Note [NASA TN D-390]: Aerodynamic characteristics of a 1/4-scale model of a tilt-wing VTOL aircraft at high angles of wing incidence
by Washington. National Aeronautics and Space Administration (NASA) | Tosti, Louis P. Material type: Book Description: 42p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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34.
|
MARKED INFLUENCE OF CRYSTAL STRUCTURE ON THE FRICTION AND WEAR CHARACTERISTICS OF COBALT AND COBALT BASE ALLOYS IN VACUUM TO 10-9 MILLIMETER OF MERCURY II-COBALT ALLOYS
by Buckley,Donlad H | Johnson,Robert L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 8.Publisher: NASA, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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35.
|
NASA TN [D-132]
: A GENERAL METHOD FOR AUTOMATIC COMPUTATION OF EQUILBRIUM COMPOSITIONS AND THEORETICAL ROCKET PERFORMANCE OF PROPELLENTS
by Gorden, Sandford | Huff,Vearl N | Zeleznik,Frank J. Description: 161p.Publisher: NASA, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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36.
|
NASA TN [D-134]
: SOME THRUST AND TRAJECTORY COSIDERRATIONS FOR LUNAR LANDINGS
by Weber,Richard J | Pauson,Werner M. Description: 37p.Publisher: NASA, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-134] (1).
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37.
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NASA Technical Note [D-135]
: FULL-SCALE WIND-TUNNEL TESTS OF A LOW-ASPECTS-RATIO, STRAIGHT-WING AIRPLANE WITH BLOWING BOUNDARY-LAYER CONTROL ON LEADING-AND TRAILING-EDGE FLAPS
by Kelly, Mark W | Maki, Ralph L | Tolhurst, William H. Description: 37p.Publisher: NASA, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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38.
|
NASA TN [D-136]
: THE EFFECTS OF THRUST REVERSAL AT MACH NUMBERS UPTO 0.86 ON THE LONGITUDINAL AND BUFFETING CHRACTERISTICS OF A TYPICAL JET-TRANSFORT AIRPLANE CONFIGURATION
by Sultton, Fred B | Brownson, Jack J. Description: 93p.Publisher: NASA, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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39.
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NASA Technical Note [NASA TN D-381]: Free-spinning-tunnel investigation of a 1/20-scale model of an unswept-wing jet-propelled trainer airplane
by Washington. National Aeronautics and Space Administration (NASA) | Bowman, James S | Healy, Frederick M. Material type: Book Description: 18p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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40.
|
NASA Technical Note [D-131]
: COMPARISON OF HDRAZINE-NITROGEN TETROXIDE AND HYDRAZINE-CHLORIDE TRIFLUORIDE IN SMALL-SCALE ROCKET CHAMBERS
by Rollbushler, R. James | Tomazic,William A. Description: 16.Publisher: NASA, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
