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Results of search for 'au:"Shaw,David S"'

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- Enderson,Laurence W (1)
- SHAW, DAVID S. (1)
- Shaw,David S (2)
- Shaw,David S,Turner,Kenneth L (1)
- Turner,Kenneth L (2)
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- PK Kelkar Library, IIT Kanpur (6)
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- PK Kelkar Library, IIT Kanpur (6)
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- Aerodynamics (1)

Your search returned 6 results.

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	1.	WIND-TUNNEL INVESTIGATION OF STATIC AERODYNAMIC CHARACTERISTICS OF A 1/9-SCALE MODEL OF A POSSIBLE REENTRY CAPSULE AT MACH NUMBERS FROM 2.29 TO 4.65 by Shaw,David S \| Turner,Kenneth L. Material type: Book Description: 19.Publisher: Nasa, Washington, D.C. 1959Availability: No items available Damaged (1). Add to cart (remove)
	2.	WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 1.60 TO 4.50 OF THE STATIC-STABILITY CHARACTURISTICS OF TWO NONLIFTING VEHICLES SUITABLE FOR REENTRY by Turner,Kenneth L \| Shaw,David S. Material type: Book Description: 34.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA MEMO 3-2-59L] (1). Add to cart (remove)
	3.	EFFECTS OF CROSS-SECTION SHAPE ON THE AERODYNAMIC CHARACTERISTICS OF BODIES AT MACH NUMBERS FROM 2.50 TO 4.63 by Fuller,Dennis E,Shaw,David S \| Wassum,Donald L. Material type: Book Description: 30.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1620] (1). Add to cart (remove)
	4.	WIND-TUNNEL INVESTIGATION OF STATIC AERODYNAMIC CHARACTERISTICS OF A1/9-SCALE MODEL OF A PROJECT MERCURY CAPSULE AT MACH NUMBERS FROM 1.60 TO 4.65 by Shaw,David S,Turner,Kenneth L. Material type: Book Description: 26.Publisher: Nasa,Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-291] (1). Add to cart (remove)
	5.	STATIC STABILITY AND SEPRATION CHRACTERISTICS A TWO-STAGE ROCKET CONFIGURATION AT MACH NUMBERS FROM 1.57 TO 4.50. by Turner,Kenneth L,Shaw,David S \| Enderson,Laurence W. Material type: Book Description: 35.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-188] (1). Add to cart (remove)
	6.	EFFECT OF NOSE BLUNTNESS,FINENESS RATIO,CONE ANGLE,AND MODEL BASE ON THE STATIC AERODYNAMIC CHARACTERISTICS OF BLUNT BODIES AT MACH NUMBER OF 1.57, 180,AND 2.16 AND ANGLE OF ATTACK UP TO 180 (DEGREE) by SHAW, DAVID S \| Babb,C. Donald \| FULLER,DENNIS E. Material type: Book Description: 77p.Publisher: NASA, WASHINGTON, D.C. 1967Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1). Add to cart (remove)

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