EKB Journal Management System

Volume & Issue: Volume 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, May 1985


1		JOUKOWSKI AIRFOIL IN SUBSONIC FLOW
	Page 1-10
	MINA B. ABD-EL-MALEK
	View Article \| PDF 1.39 MB \| View on SCiNiTO

2		Computing Lower Critical Mach Number by a Simple Method
	Page 11-15
	M. E. Essawy
	View Article \| PDF 730.05 K \| View on SCiNiTO

3		A METHOD FOR SOLVING SUPERSONIC FLOW OVER A FLAT PLATE
	Page 17-27
	M. A. ELKady; M. M. Kemry
	View Article \| PDF 2.02 MB \| View on SCiNiTO

4		AERODYNAMIC CHARACTERISTICS OF QUASI-SLENDER WING - BODY COMBINATIONS AT SUPERSONIC VELOCITIES
	Page 29-37
	O. E . ABDELHAMID
	View Article \| PDF 1.94 MB \| View on SCiNiTO

5		ALGEBRAIC PREDICTION OF TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENT
	Page 39-60
	A. M. EL-KERSH
	View Article \| PDF 3.23 MB \| View on SCiNiTO

6		Calculation Of One-Dimensional Transonic Flows Using Micro-Computers
	Page 61-70
	M. M. ABDELRAHMAN; A. O. SHERIF
	View Article \| PDF 1.44 MB \| View on SCiNiTO

7		MODELLING COMPRESSIBLE FLOW IN AXISYMMETRIC wars OF VARYING CROSS-SECTIONAL AREA
	Page 71-84
	Wafik A. Karnal; Anwar E.M. Anwar
	View Article \| PDF 2.23 MB \| View on SCiNiTO

8		NUMERICAL STUDIES OF FLOW FIELD INSIDE ENCLOSURES
	Page 85-94
	H. E.S. FATH; M. M. SOROUR
	View Article \| PDF 1.46 MB \| View on SCiNiTO

9		A STUDY OF PLANE FLOWS USING MICROCOMPUTERS
	Page 95-104
	A. O. Sherif; I. M. Shabaka
	View Article \| PDF 1.26 MB \| View on SCiNiTO

10		DESIGN OF AERODYNAMIC TEST FACILITIES
	Page 109-140
	JOHN ROSEN
	View Article \| PDF 9.84 MB \| View on SCiNiTO

11		FORCE MEASUREMENTS IN WIND TUNNELS
	Page 141-171
	K. FRISTEDT
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12		A Laser System For Cryogenic Wind Tunnels
	Page 173-181
	M. F. Essawy
	View Article \| PDF 1.98 MB \| View on SCiNiTO

13		EXPERIMENTAL INVESTIGATION ON PERFORATED CONE-CYLINDER CONFIGURATIONS IN AXISYMMETRIC SUPERSONIC FLOW
	Page 183-192
	EUGEN ERBANESCU
	View Article \| PDF 1.82 MB \| View on SCiNiTO

14		WIND TUNNEL INSTRUMENTATION TECHNIQUE BALANCE DESIGN PROBLEMS
	Page 193-200
	B. EWALD
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15		WIND TUNNEL TECHNOLOGY FOR AERONAUTICAL DEVELOPMENT PART 1 WIND TUNNEL TESTING TECHNIQUE (SURVEY; SOME SELECTED HIGHLIGHTS)
	Page 201-209
	H. P. FRANZ
	View Article \| PDF 1.88 MB \| View on SCiNiTO

16		MEASUREMENTS OF MEAN FLOW VELOCITY PROFILES OVER ROTATCNG SMOOTH AND ROUGH DISKS
	Page 211-220
	M. A. ElRefaie; M. M. Kemry; M. A. Halawa
	View Article \| PDF 2.4 MB \| View on SCiNiTO

17		AERODYNAMIC PERFORMANCE AND ASSOCIATED NOISE GENERATION SPECTRA OF AIRFOIL
	Page 221-232
	A. M. EL-KERSH; S. A. ABOU-EL-SEOUD
	View Article \| PDF 2.95 MB \| View on SCiNiTO

18		ENERGY SAVING VIA OPTIMIZATION OF AIRCRAFT FLIGHT PATH
	Page 233-243
	YEHIA A. I. ELMASHAD; GHAZY M.R. ASSASSA
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19		AN APPROACH TO THE OPTIMUM DESIGN OF THE ROTOR SYSTEM OF SINGLE-ROTOR HELICOPTERS
	Page 245-254
	M. E.I. EL-AGHA
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20		DYNAMIC STALL EFFECTS ON HELICOPTER PERFORMANCE
	Page 255-265
	E. TALAAT; M. A. KATARY
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21		PREDICTION OE STORE TRAJECTORY DROPPED 'FROM A HIGH SPEED AIRCRAFT
	Page 267-279
	M. B. KANDIEL; M. E. ESSAWf
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22		MAXIMUM FINAL ENERGY CHANDELLE FOR SUPERSONIC AIRCRAFT
	Page 281-287
	IBRAHIM MANSOUR
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23		ANALYSIS OF FULLY DEVELOPED LAMINAR CHANNEL FLOW OF SUSPENSIONS WITH EXTERNAL ELECTRIC FIELD
	Page 289-301
	S. M. ELDIGHIDY; K. A. ALBIDWEIHY
	View Article \| PDF 2.31 MB \| View on SCiNiTO

24		NON-NEWTONIAN FLUIDS FLOW THROUGH DIFFUSERS
	Page 303-312
	B. A. KHALIFA; K. IBRAHIM; M. H. EMBABY
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25		3-D STANDING WAVES IN A RECTANGULAR BASIN DUE TO A LINEAR ELASTIC RESTORING FORCE
	Page 313-328
	HELMY MUHAMMAD SAFWAT
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