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1.
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NASA Memo [10-3-58L]
: WIND-TUNNEL INVESTIGATION OF SOME EFFECTS OF WING SWEEP AND HORIZENTAL-TALL HEIGHT ON THE STATIC STABILITY OF AN AIRPLANE MODEL AT TRANSONIC SPEEDS
by Fisher, Lewis R | Williams, James L. Description: 43p.Publisher: Washington National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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2.
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NASA Memo [10-5-58L]
: SOME EFFECTS OF HORIZONTAL-TALL POSITION ON THE VERTICAL-TAIL PRESSURE DISTRIBUTIONS OF A COMPLETE MODEL IN SIDESLIP AT HIGH SUBSONIC SPEEDS
by Alford, William J. Description: 157p.Publisher: Washington National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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3.
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NASA Memo [10-8-58L]
: EFFECTS OF YAW ON THE HEAT TRANSFER TO A BLUNT CONE-CYLINDER CONFIGURATION AT A MACH NUMBER OF 1.98
by English, Roland D. Description: 20p.Publisher: Washington National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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4.
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NASA Memo [10-10-58L]
: EFFECTS OF NOSE LENGTH,FUSELAGE LENGTH,AND NOSE FINENESS RATIO ON THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF TWO COMPLETE MODELS AT HIGH SUBSONIC SPEEDS
by Goodson, Kenneth W. Description: 40p.Publisher: Washington National Aeronautics and Space Administration 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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5.
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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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6.
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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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7.
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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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8.
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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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9.
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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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10.
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LARGE-SCALE WIND-TUNNEL TESTS OF AN AIRPLANE MODEL WITH AN UNSWEPT,ASPECT-RATIO-10 WING,TWO PROPELLERS,AND BLOWING FLAPS
by Griffin,Roy N | Weiberg,James A | Holzhauser,Curt A. Material type:  Book Description: 47p.Publisher: Nasa, Washington, D.C. 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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11.
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THREE-DIMENSIONAL ORBITS OF EARTH SATELLITES,INCLUDING EFFECTS OF EARTH OBLATENESS AND ATMOSPHERIC ROTATION
by Nielsen,Jack N | Mersman,William A | Goodwin,Frederick K. Material type: Book Description: 85p.Publisher: NASA, Washington, D.C. 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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12.
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SUBSONIC AERODYNAMIC CHARACTERISTICS OF SEVERAL BLUNT,LIFTING,ATMOSPHERIC-ENTRY SHAPES
by Savage,Howard F | Tinling,Bruce E. Description: 31p.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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13.
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EFFECT OF LEADING-EDGE SWEEP AND SURFACE INCLINATION ON THE HYPERSONIC FLOW FIELD OVER A BLUNT FLAT PLATE
by Creager,Marcus O. Material type: Book Description: 45.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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14.
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EFFECT OF LOWER SURFACE SPOILERS ON THE TRANSONIC TRIM CHANGE OF A WIND-TUNNEL MODEL OF A FIGHTER AIRPLANE HAVING A MODIFIED DELTA WING
by Robinson, Robert C. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 50p.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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15.
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EFFCET OF LARGE WING-TIP MASSES ON OSCILLATORY STABILITY OF WING BENDING COUPLED WITH AIRPLANE PITCH
by Higdon,Donald T. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 32p.Publisher: NASA, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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16.
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EXPLORATORY INVESTIGATION OF THE EFFECTS OF BOUNDARY-LAYER CONTROL ON THE PRESSURE-RECOVERY CHARACTERISTICS OF A CIRCULAR INTERNAL-CONTRACTION INLET WITH TRANSLATING CENTERBODY AT MACH NUMBERS OF 2.0
by Martin, Norman J. Material type: Book Description: 44p.Publisher: NASA, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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17.
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NASA Memorandum [NASA MEMO 4-15-59A]: A flight investigation of the low-speed handling qualities of a tailless delta-wing fighter airplane
by Washington. National Aeronautics and Space Administration (NASA) | White, Maurice D | Innis, Robert C. Material type: Book Description: 33p.Publisher: Washington NASA. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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18.
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NASA Memorandum [NASA MEMO 4-18-59A]: Predicted static aeroelastic effects on wings with supersonic leading edges and streamwise tips
by Washington. National Aeronautics and Space Administration (NASA) | Brown, Stuart C. Material type: Book Description: 38p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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19.
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NASA Memorandum [NASA MEMO 4-19-59A]: Supersonic and moment-of-area rules combined for rapid zero-lift wave-drag calculations
by Washington. National Aeronautics and Space Administration (NASA) | Levy, Lionel L. Material type: Book Description: 68p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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20.
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NASA Memorandum [NASA MEMO 4-20-59A]: Static stability and control of canard configurations at mach numbers from 0.70 to 2.22- lateral-directional characteristics of an unswept wing and canard
by Washington. National Aeronautics and Space Administration (NASA) | Peterson, Victor L. Material type: Book Description: 32p.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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