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221.
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RESULTS OF A SERIES OF WIND TUNNEL MODEL BREAKDOWN TESTS ON THE TRIDENT 1 AIRCRAFT AND A COMPARISON WITH DRAG ESTIMATES AND FULL SCALE FLIGHT DATA.
by Simper,J I | Hutton,P G. Material type:  Book Description: 38.Publisher: Her Majesty'S Stationery Office, London 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P. 1170] (1).
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222.
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THE SHEAR STIFFNESS OF A CORRUGATED WEB.
by Mckenzie,K I. Material type: Book Description: 13.Publisher: Her Majesty'S Stationery Office, London 1963Availability: No items available Damaged (1).
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223.
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AN ANALYSIS OF TWO-DIMENSIONAL TURBULENT BASE FLOW,INCLUDING THE EFFECT OF THE APPROACHING BOUNARY LAYER.
by Nash,J F. Material type: Book Description: 39.Publisher: Her Majesty'S Stationery Office, London 1963Availability: No items available Damaged (1).
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224.
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A FLIGHT STUDY OF THE SIDESTEP MANOEUVRE DURING LANDING.
by Perry,D H,Port,W G | Morrall.,J C. Material type: Book Description: 50.Publisher: Her Majesty'S Stationery Office, London 1064Availability: No items available Damaged (1).
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225.
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TESTS AT TRANSONIC SEEPDS OD WINGS WITH WEDGE SECTIONS AND SWEEP VARYING BETWEEN 0 DEGREE AND 60 DEGREE
by Rogers,E W.E,Berry,C J. Material type: Book Description: 104.Publisher: Her Majesty'S Stationery Office, London 1963Availability: No items available Damaged (1).
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226.
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THE USE OF SURFACE PITOT TUBES AS SKIN-FRICTION METERS AT SUPERSONIC SPEEDS.
by Smith,K G,Gaudet,L | Winter,K G. Material type: Book Description: 36.Publisher: Her Majesty'S Stationery Office, London 1964Availability: No items available Damaged (1).
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227.
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A NOTE ON THE THEORY OF PARACHUTE STABILITY.
by Lester,W G.S. Material type: Book Description: 15.Publisher: Her Majesty'S Stationery Office, London 1964Availability: No items available Damaged (1).
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228.
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THE ESTIMATION OF STRESSES AROUND UNREINFORCED HOLES IN INFINITE ELASTIC SHEETS.
by Sobey,A J. Material type: Book Description: 18.Publisher: Her Majesty'S Stationery Office, London 1964Availability: No items available Damaged (1).
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229.
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OSCILLATORY-DERIVATIVE MEASUREMENTS ON STINGMOUNTED WING-TUNNEL MODELS
: METHOD OF TEST AND RESILTS FOR PITCH AND YAW ON A CAMBERED OGEE WING AT MACH NUMBERS UP TO 2.6
by Thompson,J S | Fail,R A. Material type: Book Description: 52.Publisher: Her Majesty'S Stationery Office, London 1964Availability: No items available Damaged (1).
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230.
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QUALITATIVE SOLUTION OF THE STABILITY EQATION FOR A BOUNDARY LAYER IN CONTACT WITH VARIOUS FORMS OF FLEXIBLE SURFACE.
by Nonweiler,T. Material type: Book Description: 59.Publisher: Her Majesty'S Stationery Office, London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C. P. 622] (1).
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231.
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NOTES ON SOME EXPERIMENTAL AND THEORETICAL RESULTS FOR THE BOUNDARY LAYER DEVELOPMENT AFT OF THE SHOCK IN A SHOCK-TUBE.
by Bernstein,L. Material type: Book Description: 32.Publisher: Her Majesty'S Stationery Office, London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P. 625] (1).
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232.
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.TABULATED SOLUTIONS OF THE EQUILIBRIUM GAS PROPERTIES BEHIND THE INCIDENT AND REFLECTED NORMAL SHOCK-WAVE IN A SHOCK-TUBE I-NITROGEN II-OXYGENE
by Bernstein,L. Material type: Book Description: 64.Publisher: Her Majesty'S Stationery Office, London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P. 626] (1).
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233.
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AN INVESTIGATION OF WING-AILERON FLUTTER USING GROUND LAUNCHED ROCKET MODELS.
by Gaukroger,D R | Curran,J K. Material type: Book Description: 15.Publisher: Her Majesty'S Stationery Office, London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P. 627] (1).
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234.
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THE CALIBRATION OF A 60 DEGREE CONE TO MEASURE MACH NUMBER, TOTAL PRESSURE AND FLOW ANGLES AT SUPERSONIC SPEEDS.
by Andrews,D R | Sawyer,W G. Material type: Book Description: 10.Publisher: Her Majesty'S Stationery Office, London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P. 628] (1).
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235.
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AERODYNAMIC AND MECHANICAL TESTS OF A MODEL OF A VARIABLE MACH NUMBER NOZZLE.
by Jawor,Z M. Material type: Book Description: 7.Publisher: Her Majesty'S Stationery Office, London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P 629] (1).
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236.
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SOME CHARACTERISTICS OF RECTANGULAR MULTI-SHOCK AND ISENTROPIC EXTERNAL COMPRESSION INTAKES AT A MACH NUMBER OF 2.9
by Dutton,R A | Goldsmith,E L. Material type: Book Description: 12.Publisher: Her Majesty'S Stationery Office, London 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P. 630] (1).
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237.
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FLIGHT AND TUNNEL MEASUREMENTS OF PRESSURE FLUCTATIONS ON THE UPPER SURFACE OF THE WING OF A VENOM AIRCRAFT WITH A SHARPENED LEADING-EDGE.
by Rose,R | Nicholas,O P. Material type: Book Description: 32.Publisher: Her Majesty'S Stationery Office, London 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC-C.P 1032] (1).
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238.
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A METHOD FOR THE PREDICTION OF THE PROBABILITIES OF AIRCRAFT FATIGUE FAILURES WITHIN A FLEET OF KNOWN SIZE.
by Stagg,A M. Material type: Book Description: 30.Publisher: Her Majesty'S Stationery Office, London 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC-C.P 1033] (1).
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239.
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ANALYSIS OF SOME MAJOR FACTORS INVOLVED IN NORMAL TAKE-OFF PERFORMANCE.
by Perry,D H. Material type: Book Description: 52.Publisher: Her Majesty'S Stationery Office, London 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC-C.P 1034] (1).
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240.
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CALCULATION OF THE REPONSE OF A TRANSPORT AIRCRAFT TO CONTINUEOUS TURBULENCE AND DISCRETE GUSTS AND A COMPARISON WITH FLIGHT MEASUREMENTS.
by Mitchell,C G.B. Material type: Book Description: 29.Publisher: Her Majesty'S Stationery Office, London 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC-C.P 1035] (1).
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