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5821.
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NONVISCOUS FLOW THROUGH A PUMP IMPELLER ON A BLADE- TO BLADE SURFACE OF REVOLUTION
by Kramer,James J,Stockman,Norbert O | Bean,Ralph J. Material type:  Book Description: 29.Publisher: Nasa, Washington, D.C. 1962Availability: No items available Damaged (1).
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5822.
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INVESTIGATION OF THE PERFORMANCE OF AN AXIAL-FLOW-PUMP STAGE DESIGNED BY THE BLADE-ELEMENT THEORY-BLADE-ELEMENT DATA
by Crouse,James E,Soltis,Richard F | Montgomery,John C. Material type: Book Description: 66.Publisher: Nasa, Washington, D.C. 1961Availability: No items available Damaged (1).
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5823.
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A PARAMETRIC STUDY OF THE THERMIONIC DIODE SYSTEM FOR LARGE NUCLEAR-ELECTRIC POWERPLANTS IN SPACE VEHICLES
by Bernatowicz,Daniel T. Material type: Book Description: 53.Publisher: Nasa, Washington, D.C. 1962Availability: No items available Damaged (1).
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5824.
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BALLOON TANK SKIN STRAIN MEASUREMENTS AT LIQUID-HYDROGEN TEMPERATURE ON CENTAUR FLIGHT VEHICLE
by Lall,Tilak R,Maruna,Frank A | Lang,William F. Material type: Book Description: 19.Publisher: Nasa, Washington, D.C. 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-1147] (1).
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5825.
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SELECTIVE ELECTROPLATING OF ETCHED CIRCUITS
by Whitfield,Charles E | Herzig,Howard. Material type: Book Description: 4.Publisher: Nasa, Washington, D.C. 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-1168] (1).
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5826.
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EFFECTS OF TRANSIENT HEATING ON THE VIBRATION FREQUENCIES OF A PROTOTYPE OF THE X-15 WING
by Mcwithey,Robert R | Vosteen,Louis F. Material type: Book Description: 21.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-362] (1).
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5827.
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INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A COMBINATION JET-FLAP AND DEFLECTED-SLIPSTREAM CONFIGURATION AT ZERO AND LOW FORW ARD SPEEDS
by Spreemann,Kenneth P | Davenport,Edwin E. Material type: Book Description: 72.Publisher: Nasa, Washington, D.C. 1960Availability: No items available Damaged (1).
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5828.
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FLIGHT MEASUREMENTS OF THE EFFECTS OF BLADE OUT OF TRACK ON THE VIBRATION LEVELS ON A TANDEM ROTOR HELICOPTER
by Ludi,Leroy H | Yeates,John E. Material type: Book Description: 26.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-364] (1).
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5829.
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SHOCK-WAVE STRUCTURE BASED ON IKENBERRY-TRUESDELL APPROACH TO KINETIC THEORY OF GASES
by Street,Robert E. Material type: Book Description: 60.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-365] (1).
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5830.
|
POSSIBLE EFFECTS OF NONUNIFORM FLOWS ON PERFORMANCE OF ELECTROTHERMAL THRUSTORS
by Jack,John R,Schaefer,John W. Material type: Book Description: 16.Publisher: Nasa,Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1732] (1).
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5831.
|
NEUTRALIZER TESTS ON A FLIGHT-MODEL ELECTRON-BOMBARDMENTION THRUSTOR
by Kemp,Robert F,Sellen,J M. Material type: Book Description: 37.Publisher: Nasa,Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1733] (1).
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5832.
|
DISPERSION AND DAMPING OF LONGITUDINAL ELECTRON OSCILLATIONS IN THERMAL PLASMA
by Morris,James F. Material type: Book Description: 56.Publisher: Nasa,Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1734] (1).
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5833.
|
TABLE OF2 F1 (A,B;C;Z) FOR A=0(1/2)7, B(1/2)7, AND C=0(1/2)5/2 WITH COMMENTS ON CLOSED FORMS OF2F1 ( A,B;C;Z )
by Steidley,K David. Material type: Book Description: 26.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA 1735] (1).
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5834.
|
WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER
by Pearson,Albin O. Material type: Book Description: 63.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-317] (1).
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5835.
|
AERODYNAMIC CHARACTERISTICS AT MACH NUMBER 2.05 OF A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER
by Carlson,Harry W. Material type: Book Description: 34.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-332] (1).
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5836.
|
PRESSURE DISTRIBUTION ON TWO MODELS OF A PROJECT MERCURY CAPSULE FOR A MACH NUMBER RANGE OF 1.60 TO 6.01 AND AN ANGLE-OF-ATTACK RANGE OF 0 DEGREE TO 180 DEGREE
by Newlander,Robert A,Taylor,Nancy L | Pritchard,E Brian. Material type: Book Description: 96.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-336] (1).
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5837.
|
SOME AERODYNAMIC AND CONTROL STUDIES OF LIFTING REENTRY COFIGURATIONS AT ANGLES OF ATTACK UP TO 90 DEGREE AT A MACH NUMBER OF 2.91
by Clark,Frank L | Evans,Joanna M. Material type: Book Description: 48.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-338] (1).
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5838.
|
BASIC PRESSURE MEASUREMENTS ON A 0.0667-SCALE MODEL OF THE NORTH AMERICAN X-15 RESEARCH AIRPLANE AT TRANSONIC SPEEDS
by Osborne,Robert S | Stafford,Virginia C. Material type: Book Description: 101.Publisher: Nasa, Washington, D.C. 1960Availability: No items available Damaged (1).
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5839.
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LOW-SUBSONIC MEASUREMENTS OF THE STATIC STABILITY AND CONTROL AND OSCILLATORY STABILITY DERIVATIVES OF A PROPOSED REENTRY VEHICLE HAVING AN EXTENSIBLE HEAT SHIELD FOR HIGH-DRAG REENTRY
by Johnson,Joseph L | Boisseau,Peter C. Material type: Book Description: 35.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-892] (1).
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5840.
|
POWER SPECTRAL ANALYSIS OF SOME AIRPLANE RESPONSE QUANTITIES OBTAINED DURING OPERATIONAL TRAINING MISSIONS OF A FIGHTER AIRPLANE
by Hamer,Harol A | Mayer,John P. Material type: Book Description: 41.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-366] (1).
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