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EFFECTS OF BODY SHAPE ON THE DRAG OF A 45DEGREE OFSWEPTBACK-WING-BODY CONFIGURATION AT MACH NUMBERS FROM 0.90 TO 1.43.

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BookPublisher: Nasa, Washington, D.C. 1958Description: 67.DDC classification: NASA | MEMO 10-23-58L

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA MEMO 10-23-58L (Browse shelf)	Not for loan Untraceable		TR11151

Total holds: 0

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Previous	NASA D-646 LOW-SUBSONIC-SPEED STATIC STABILITY OF RIGHT-TRIANGULAR-PYRAMID AND HALF-CONE LIFTING REENTRY CONFIGURATIONS	NASA MEMO 10-19-58L STATIC INVESTIGATION OF PADDLE VANE OSCILLATING IN JET OF 1,300-POUND-THRUST ROCKET MOTOR.	NASA MEMO 10-22-58L LOW-SPEED STATIC STABILITY CHARACTERISTICS OF TWO CONFIGERATIONS SUITABLE FOR LIFTING REENTRY FROM SATELLITE ORBIT.	NASA MEMO 10-23-58L EFFECTS OF BODY SHAPE ON THE DRAG OF A 45DEGREE OFSWEPTBACK-WING-BODY CONFIGURATION AT MACH NUMBERS FROM 0.90 TO 1.43.	NASA MEMO 10-25-58L HEAT-TRANSFER MEASUREMENTS OF TWO WING-BODY COMBINATIONS AT *DEGREE ANGLE OF ATTACK FROM A FLIGHT TEST FOR MACH NUMBERS TO 4.86 AND REYNOLDS NUMBERS TO 19.2	NASA MEMO 10-26-58L FLIGHT INVESTIGATION OF A NORMAL-ACCELERATION AUTOMATIC LONGITUINAL CONTROL SYSTEM IN A FIGHTER AIRPLANE	NASA MEMO 10-27-58L HOVERING AND TRANSITION FLIGHT TESTS OF A 1/5-SCALE MODEL OF JET-POWERED VERTICAL-ATTITUDE VTOL RESEARCH AIRPLANE.	Next

Bound With:Nasa Memo 10-18-58l-10-22-58l,10-24-58l-10-28-59l..Lack No10-21-58l,10-24-58l.

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