|
|
221.
|
THE ACCELERATION OF WATER DROPS BY AN AIRSTREAM OF CONSTANT RELATIVE VELOCITY.
by Jenkins,D C. Material type:  Book Description: 9.Publisher: Her Majesty'S Stationery Office, London 1961Availability: No items available Damaged (1).
|
|
|
222.
|
A METHOD FOR DESIGNING BODY SHAPE TO PRODUCE PRESCRIBED PRESSURE DISTRIBUTIONS ON WING-BODY COMBINATIONS AT SUPERSONIC SPEEDS.
by Jones,J G. Material type: Book Description: 36.Publisher: Her Majesty'S Stationery Office, London 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P. 540] (1).
|
|
|
223.
|
ON THE INTERACTION OF THE TRANSMITTED SHOCK WITH THE BOUNDARY LAYER IN A SHOCK TUBE USING ARGON AS A TEST GAS.
by Devies,L | Bridgman,K. Material type: Book Description: 9.Publisher: Her Majesty'S Stationery Office, London 1967Availability: No items available Damaged (1).
|
|
|
224.
|
ASEMI-EMPIRICAL PREDICTION METHOD FOR PRESSURE ON THE WINDWARD SURFACE OF CIRCULAR CONES AT INCIDENCE AT HIGH SUPERSONIC AND HYPERSONIC SPEEDS (M>3)
by Collingbourne,J R,Crabtree,L F | Bartlett,W J. Material type: Book Description: 15.Publisher: Her Majesty'S Stationery Office, London 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: ARC C.P. 792] (1).
|
|
|
225.
|
EFFECT OF FLOW CURVATURE DUE TO THE FUSELAGE ON THE FLAPPING MOTION OF A HELICOPTER ROTOR.
by Willmer,Map. Material type: Book Description: 11.Publisher: Her Majesty'S Stationery Office, London 1965Availability: No items available Damaged (1).
|
|
|
226.
|
THE CHANGE OF PITOT PRESSURE ACROSS OBLIQUE SHOCK WAVES IN A PERFECT GAS.
by Graham,W J | Davis,B M. Material type: Book Description: 2.Publisher: Her Majesty'S Stationery Office, London 1965Availability: No items available Damaged (1).
|
|
|
227.
|
MACH NUMBER DISTRIBUTIONS ALONG THE SLOTTED WALLS OF THE N.P.L. 20 IN. *8 IN. HIGH-SPEED WIND TUNNEL
by Pearcey,H H | Regan,J D. Material type: Book Description: 6.Publisher: Her Majesty'S Stationery Office, London 1965Availability: No items available Damaged (1).
|
|
|
228.
|
ATMOSPHERIC TURBULENCE ENCOUNTERED BY HERMES AIRCRAFT ON ROUTES TO AFRICA AND THE FAR EAST.
by Aplin,Judy E. Material type: Book Description: 23.Publisher: Her Majesty'S Stationery Office, London 1965Availability: No items available Damaged (1).
|
|
|
229.
|
EFFECTS OF VARIED LOADING PATHS ON FATIGUE ENDURANCES.
by Tilly,G P. Material type: Book Description: 27.Publisher: Her Majesty'S Stationery Office, London 1965Availability: No items available Damaged (1).
|
|
|
230.
|
EFFECTS OF VARIED LOADING PATHS ON FATIGUE ENDURANCES.
by Tilly,G P. Material type: Book Description: 17.Publisher: Her Majesty'S Stationery Office, London 1965Availability: No items available Damaged (1).
|
|
|
231.
|
EFFECTS OF VARIED LOADING PATHS ON FATIGUE ENDURANCES.
by Tilly,G. P. Material type: Book Description: 24.Publisher: Her Majesty'S Stationery Office, London 1965Availability: No items available Damaged (1).
|
|
|
232.
|
PROPOSALS FOR AN INTEGRATED WIND TUNNEL-FLIGHT DYNAMICS SIMULATOR SYSTEM.
by Beecham,L J,Walters,W L | Partridge,D W. Material type: Book Description: 21.Publisher: Her Majesty'S Stationery Office, London 1965Availability: No items available Damaged (1).
|
|
|
233.
|
EFFECT ON THE STATIC STRENGTH OF ALUMINIUM ALLOY TEST SPECIMENS OF THE ATTACHMENT OF THERMOCOUPLES BY A WELDING TECHNIQUE.
by Wright,D F | Acheson,G F. Material type: Book Description: 27.Publisher: Her Majesty'S Stationery Office, London 1965Availability: No items available Damaged (1).
|
|
|
234.
|
LOADING CONDITIONS OF TAILED AIRCRAFT IN LONGITUDINAL MANOEUVRES.
by Czaykowski,T. Material type: Book Description: 59.Publisher: Her Majesty'S Stationery Office, London 1956Availability: No items available Damaged (1).
|
|
|
235.
|
FLOW IN THE LAMINAR BOUNDARY LAYER NEAR SEPERATION.
by Stratford,B S. Material type: Book Description: 27.Publisher: Her Majesty'S Stationery Office, London 1957Availability: No items available Damaged (1).
|
|
|
236.
|
THE INTERACTION BETWEEN SHOCK WAVES AND BOUNDARY LAYERS AT THE TRAILING EDGE OF A DOUBLE-WEDGE AEROFOIL AT SUPERSONIC SPEED.
by Henshall,B D | Cash,R F. Material type: Book Description: 10.Publisher: Her Majesty'S Stationery Office, London 1957Availability: No items available Damaged (1).
|
|
|
237.
|
EFFECT OF YAW ON THE COMPRESSIBLE LAMINAR BOUNDARY LAYER.
by Tinkler,J. Material type: Book Description: 14.Publisher: Her Majesty'S Stationery Office, London 1957Availability: No items available Damaged (1).
|
|
|
238.
|
THE THREE-DIMENSIONAL BOUNDARY-LAYER EQUATIONS AND SOME POWER SERIES SOLUTIONS.
by Squire,L C. Material type: Book Description: 17.Publisher: Her Majesty'S Stationery Office, London 1957Availability: No items available Damaged (1).
|
|
|
239.
|
THE EFFECT OF A SPIKE PROTRUDING IN FRONT OF A BLUFF BODY AT SUPERSONIC SPEEDS.
by Beastall,D | Turner,J. Material type: Book Description: 26.Publisher: Her Majesty'S Stationery Office, London 1957Availability: No items available Damaged (1).
|
|
|
240.
|
VELOCITY DISTRIBUTION ON THIN TAPERED ARROWHEAD AND DELTA WINGS WITH SPANWISE CONSTANT THICKNESS RATIO AT ZERO INCIDENCE.
by Neumark,S,Collingbourne,J | York,E J. Material type: Book Description: 18.Publisher: Her Majesty'S Stationery Office, London 1958Availability: No items available Damaged (1).
|
