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61.
|
NASA TN [D-4146]
: PRELIMINARY DETERMINATIONS OF TEMPERATURE LIMITATIONS OF ESTER, ETHER AND HYDROCARBON BASE LUBRICANTS IN 25-MM BORE BALL BEARINGS
by Zaretsky, Erwin V | Anderson, William J. Description: 21p.Publisher: Washington National Aeronautics and Space Administration 1967Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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62.
|
NASA TN [D-4148]
: PERFORMANCE POTENTIAL OF A RADIANT-HEAT-TRANSFER LIQUID-CORE NUCLEAR ROCKET ENGINE
by Ragsdale, Robert G. Description: 25p.Publisher: Washington National Aeronautics and Space Administration 1967Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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63.
|
NASA TN [D-4149]
: MIST-FLOW HEAT TRANSFER USING SINGLE-PHASE VARIABLE-PROPERTY APPROACH
by Hsu,Yih-Yun | Cowgill, Glenn R | Hendricks, Robert C. Description: 78p.Publisher: Washington National Aeronautics and Space Administration 1967Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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64.
|
A SEROCONTROLLER FOR PROGRAMMING SAMPLE VAPORIZATION IN DIRECT CURRENT ARC SPECTROCHEMICAL ANALYSIS [NASA TN D-4769]
by Gordon, William A. Material type:  Book; Format:
print
; Literary form:
not fiction
Description: 31p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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65.
|
ANALOG COMPUTER SIMULATION OF A DC ARC EMISSION SPECTROMETER CONTROL SYSTEM TO DEFINE REQUIREMENTS FOR OPTIMUM CONTROL [NASA TN D-4770]
by Lesco, Daniel J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 23p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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66.
|
COMPUTER PROGRAM FOR SYSTEMATICALLY ANALYZING FREE-FLIGHT DATA TO DETERMINE THE AERODYNAMICS OF AXISYMMETRIC BODIES [NASA TN D-4766]
by Malcolm,Gerald N | Chapman,Gary T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 37p.Publisher: Washington, D.C National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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67.
|
TESTS OF A SINGLE TUBE-IN-SHELL WATER-BOILING HEAT EXCHANGER WITH A-WIRE INSERT AND SEVERAL INLET FLOW-STABILIZING DEVICES [NASA TN D-4767]
by Stone, James R | Dekas,Nick J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 59.Publisher: Washington, D.C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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68.
|
ATMOSPHERIC CONDITIONS ASSOCIATED WITH TURBULENCE ENCOUNTERED BY THE XB-70 AIRPLANE ABOVE 40,000 FEET ALTITUDE [NASA TN D-4768]
by Ehernberger, L. J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 47p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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69.
|
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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70.
|
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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71.
|
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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72.
|
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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73.
|
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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74.
|
AERODYNAMIC-DERIVATIVE CHARACTERISTICS OF THE X-15 RESEARCH AIRPLANE AS DETERMINED FROM FLIGHT TESTS FOR MACH NUMBERS FROM 0.6 TO 3.4 [NASA TN D-1010]
by Yancey, Roxaanah B. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 68p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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75.
|
TRANSONIC WIND-TUNNEL INVESTIGATION OF THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL CONFIGURATIONS OF THE SCOUT VEHICLE AND OF A NUMBER OF RELATED MODELS [NASA TN D-794]
by Kelly, Thomas C. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 69p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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76.
|
A SEMIGRAPHICAL METHOD OF APPLYING IMPACT THEORY TO AN ARBITRARY BODY TO OBTAIN THE HYPERSONIC AERODYNAMIC CHARACTERISTICS AT ANGLE OF ATTACK AND SIDESLIP [NASA TN D-795]
by Jackson, Charlie M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 18p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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77.
|
Residual static strength of aluminium alloy box beams containing fatigue cracks in the tension covers [NASA TN D-796]
by Leybold, Herbert A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 25p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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78.
|
Theoretical evaluation of hypersonic forces, moments, and stability derivatives for a combination of flat plates, including effects of blunt leading edges by Newtonian impact theory[NASA TN D-1015]
by Olstad,Walter B. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 66p.Publisher: Washington, D.C. National Aeronautics and Space Administration Washington 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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79.
|
DETAILED PERFORMANCE OF A RADIAL-BLADED CENTRIFUGAL PUMP IMPELLER IN WATER [NASA TN D-4613]
by Miller, Max J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 52p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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80.
|
BODY ROTATION EFFECTS ON MELTING ABLATION [NASA TN D-4614]
by Cochran, Thomas H. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 39p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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