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121.
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ON THE INTEGRAL EQUATIONS OF TWO-DIMENSIONAL SUBSONIC FLUTTER DERIVATIVE THEORY
by Williams,D. E. Material type:  Book Description: 21.Publisher: Her Majesty'S Stationery Office,London 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3057 -] (1).
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122.
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ACCURACY OF MEASURMENT OF TURBULENT SKIN FRICTION BY MEANS OF SURFACE PITOT-TUBES AND THE DISTRIBUTION OF SKIN FRICTION ON A FLAT PLATE
by Dutton,R. A. Material type: Book Description: 18.Publisher: Her Majesty'S Stationery Office,London 1957Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3058 -] (1).
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123.
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CALCULATION OF DERIVATIVES FOR A CROPPED DELTA WING WITH AN OSCILLATING CONSTANT-CHORD FLAP IN A SUPERSONIC AIR STREAM
by Watson,J. Material type: Book Description: 34.Publisher: Her Majesty'S Stationery Office, London 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3059 -] (1).
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124.
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CALCULATION OF DERIVATIVES FOR A CROPPED DELTA WING WITH SUBSONIC LEADING EDGES OSCILLATING IN A SUPERSONIC AIR STREAM
by Watson,J. Material type: Book Description: 34.Publisher: Her Majesty'S Stationery Office,London 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3060 -] (1).
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125.
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NOTE ON THE CONVERGENCE OF NUMERICAL SOULITIONS OF THE NAVIER-STROKES EQUATIONS
by Thom,A., Apelt,C. J. Material type: Book Description: 8.Publisher: Her Majesty'S Stationery Office,London 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3061 -] (1).
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126.
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EXPERIMENTAL INVESTIGATION OF THE EFFECT OF ENGINE LOADS ON WING STRUCTURES
by Reddaway,J. L. Material type: Book Description: 15.Publisher: Her Majesty'S Stationery Office,London 1957Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3062 -] (1).
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127.
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SAMPLING ERRORS OF ATMOSPHERICTURBULENCE MEASUREMENTS
by Bullen,N I. Material type: Book Description: 14.Publisher: Her Majesty'S Stationery Office, London 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3063 -] (1).
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128.
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EXPERIMENTS ON TWO-DIMENSIONAL BASE FLOW AT M = 2.4
by Fuller,L | Reid,J. Material type: Book Description: 34.Publisher: Her Majesty'S Stationery Office, London 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3064 -] (1).
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129.
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EFFECT OF WING-TAILPLANE AERODYNAMIC INTERACTION ON TAIL FLUTTER
by Williams,D. E. Material type: Book Description: 24.Publisher: Her Majesty'S Stationery Office, London 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3065 -] (1).
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130.
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SUPERSONIC FLOW PAST QUASI-CYLINDRICAL BODIES OF ALMOST CIRCULAR CROSS-SECTION
by Randall,D. G. Material type: Book Description: 17.Publisher: Her Majesty'S Stationery Office, London 1958Availability: No items available Damaged (1).
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131.
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CALCULATED DERIVATIVES FOR RECTANGULAR WINGS OSCILLATING IN COMPRESSIBLE SUBSONIC FLOW
by Lehrian,Doris E. Material type: Book Description: 15.Publisher: Her Majesty'S Stationery Office, London 1958Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3068 -] (1).
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132.
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OPTICS OF THE MACH-ZEHNDER INTERFEROMETER
by Tanner,L. H. Material type: Book Description: 62.Publisher: Her Majesty'S Stationery Office, London 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-3069 -] (1).
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133.
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CALCULATION OF DERIVATIVES FOR A CROPPED DELTA WING WITH AN OSCILLATING CONSTANT-CHORD FLAP IN A SUPERSONIC AIR STREAM
by Watson,J. Material type: Book Description: 34.Publisher: Her Majesty'S Stationery Office,London 1958Availability: No items available Damaged (1).
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134.
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STATIC AND DYNAMICS RESPONSE PROPERTIES OF INCIDENCE VANES WITH AERODYNAMIC AND INTERNAL VISCOUS DAMPING
by Pinsker,W. J. G. Material type: Book Description: 16.Publisher: Her Majesty'S Stationery Office,London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-652 -] (1).
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135.
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FLIGHT MEASUREMENTS OF THE DUTCH ROLL CHARACTERISTICS OF A 60 DEGREE DELTA WING AIRCRAFT (FAIREY DELTA 2) AT MACH NUMBERS FROM 0.4 TO 1.5 WITH STABILITY DERIVATIVES EXTRACTED BY VECTOR ANALYSIS
by Rose,R. Material type: Book Description: 26.Publisher: Her Majesty'S Stationery Office,London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-653 -] (1).
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136.
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CALCULATION OF THE VELOCITY DISTRIBUTION DUE TO THICKNESS FOR SWEPT WINGS WITH SUBSONIC EDGES AT SUPERSONIC SPEEDS
by Haines,A. B., Rollins,K | Osborn,J. Material type: Book Description: 38.Publisher: Her Majesty'S Stationery Office,London 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-654 -] (1).
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137.
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PROPAGATION OF FATIGUE CRACKS IN WIDE UNSTIFFENED ALUMINIUM ALLOY SHEETS
by Raithby,K. D., Bebb,Marie E. Material type: Book Description: 18.Publisher: Her Majesty'S Stationery Office,London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-655 -] (1).
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138.
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8FT. X 6FT. TRANSONIC WIND TUNNEL TESTS ON A 1/24 SCALE MODEL OF THE FAIREY DELTA 2 (ER.103)
by Kettle,D. J. Material type: Book Description: 42.Publisher: Her Majesty'S Stationery Office, London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: HMSO-R&M-656 -] (1).
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139.
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NATURE, DEVLOPMENT AND EFFECT OF THE VISCOUS FLOW AROUND AN AEROFOIL WITH HIGH-LIFT DEVICES
by Foster,D. N., Ashill,P. R | Williams,B. R. Material type: Book Description: 29.Publisher: Her Majesty'S Stationery Office, London 1974Availability: No items available Damaged (1).
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140.
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FATIQUE ENDURANCE, CRACK SENSITIVITY AND NUCLEATION CHARACTERISTICS OF STRUCTURAL ELEMENTS IN FOUR ALUMINIUM-COPPER ALLOYS
by Kiddle,F. E. Material type: Book Description: 52.Publisher: Her Majesty'S Stationery Office, London 1974Availability: No items available Damaged (1).
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