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21.
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NASA Technical Note [NASA TN D-3442]: Low-subsonic wind-tunnel and free-flight drop-test investigation of a paraglider configuration having large tapered leading edges and keel
by Washington. National Aeronautics and Space Administration (NASA) | Croom, Delwin R | Fournier, Paul G. Material type:  Book Description: 32p.Publisher: Washington NASA 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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22.
|
ION-THRUSTER PROPELLANT UTILIZATION
by Kaufman,Harold R. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 56p.Publisher: NASA, Washington, D.C. 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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23.
|
MIXING OF SUPERSONIC JETS INCLUDING THE EFFECTS OF TRANSVERSE PRESSURE GRADIENT USING DIFFERENCE METHODS
by Kurkov, Anatole P. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 30p.Publisher: NASA, Washington, D.C. 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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24.
|
FIELD EVAPORATION ION SOURCE WITH POSSIBLE APPLICATION TO ELECTROSTATIC PROPULSION
by Weizer, Victor G. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 20p.Publisher: NASA, Washington, D.C. 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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25.
|
HEAT TRANSFER AND BOUNDARY LAYER IN CONICAL NOZZLES
by Boldman,Donald R | Graham,Robert W. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 59p.Publisher: NASA, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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26.
|
NASA Technical Note [NASA TN D-2546]: Use of arbitrary quasi-orthogonals for calculating flow distribution in the meridional plane of a turbomachine
by Washington. National Aeronautics and Space Administration (NASA) | Katsanis, Theodore. Material type: Book Description: 46p.Publisher: Washington NASA 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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27.
|
NASA Technical Note [NASA TN D-3122]: Performance characteristics of a 4-foot-diameter ducted fan at zero angle of attack for several fan blade angles
by Washington. National Aeronautics and Space Administration (NASA) | Mort, Kenneth W. Material type: Book Description: 17p.Publisher: Washington NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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28.
|
NASA Technical Note [NASA TN D-3126]: Strain measurements conducted on a full scale echo ii passive communications satellite balloon
by Washington. National Aeronautics and Space Administration (NASA) | Staugaitis, Charles L | Kobren, Lawrence. Material type: Book Description: 23p.Publisher: Washington NASA 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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29.
|
NASA Memo [10-2-58L]
: AERODYNAMIC CHARACTERISTICS FOR COMBINED ANGLES OF ATTACK AND SIDESLIP OF A LOW-ASPECT-RATIO CRUCIFORM-WING MISSILE CONFIGURATION EMPLOYING VARIOUS CANARD AND TRAILING-EDGE FLAP CONTROLS AT A NO.2.01
by Robinson, Ross B | Spearman, M. Leroy. Description: 71p.Publisher: Washington National Aeronautics and Space Administration 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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30.
|
NASA Technical Note [NASA TN D-5932]: Full-scale wind-tunnel investigation of the aerodynamic characteristics of the x-24a lifting body aircraft
by Washington. National Aeronautics and Space Administration (NASA) | Mort, Kenneth W | Falarski, Michael D. Material type: Book Description: 54p.Publisher: Washington NASA 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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31.
|
NASA Memo [10-11-58L]
: AERODYNAMIC CHARACTERISTICS IN SIDESLIP OF A LARGE-SCALE 49(DEGREE) SWEPTBACK WING-BODY-TAIL CONFIGURATION WITH BLOWING APPLIED OVER THE FLAPS AND WING LEADING EDGE
by Mclemore, H. Clyde. Description: 46p.Publisher: Washington National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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32.
|
NASA Memo [10-12-58L]
: TESTS OF AERODYNAMICALLY HEATED MULTIWEB WING STRUCTURES IN A FREE JET AT MACH NUMBER 2 : THREE MODELS OF 20-INCH CHORD AND SPAN CONSTRUCTED FROM MAGNESIEUM, TITANIUM, AND ALUMINUM ALLOYS, RESPECTIVELY
by Davidson, John R | Rosecrans, Richard. Description: 23p.Publisher: Washington National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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33.
|
NASA Memo [10-13-58L]
: LOW-SPEED AERODYNAMIC AND HYDRODYNAMIC CHARACTERISTICS OF A PROPOSED SUPERSONIC MULTIJET WATER-BASED HYDRO-SKI AIRCRAFT WITH UPWARD-ROTATING ENGINES
by Petynia, William W | Croom, Delwin R | Davenport, Edwin E. Description: 59p.Publisher: Washington National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
|
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34.
|
NASA Memo [10-13-58L]
: FLUTTER TESTES OF SANDWICH-TYPE FLAT PANELS AT MACH NUMBERS OF 2.97 AND 4.12
by Kordes, Eldon E | Evans, Ernest W. Description: 16p.Publisher: Washington National Aeronautics and Space Administration 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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35.
|
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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36.
|
NASA Technical Note [NASA TN D-2547]: Energy transfer from a liquid to gas bubbles forming at a submerged orifice
by Washington. National Aeronautics and Space Administration (NASA) | L'Ecuyer, M. R | Murthy, S. N. B. Material type: Book Description: 178p.Publisher: Washington NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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37.
|
NASA Technical Note [NASA TN D-2550]: Application of generalized Newtonian theory to three-dimensional sharp-nose shock-detached bodies at mach for angles of attack up to 25 [degree]
by Washington. National Aeronautics and Space Administration (NASA) | Ashby, George C | Goldberg, Theodore J. Material type: Book Description: 41p.Publisher: Washington NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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38.
|
NASA Technical Note [NASA TN D-446]: Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag
by Washington. National Aeronautics and Space Administration (NASA) | Nelson, Robert L | Welsh, Clement J. Material type: Book Description: 46p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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39.
|
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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|
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40.
|
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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