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Results of search for 'au:"Sleeman,William C"'

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Authors
- Bugg, Frank M. (1)
- Fournier,Paul G (1)
- Polhamus,Edward C (1)
- Sleeman,William C (4)
- Spencer,Bernard (1)
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Holding libraries
- PK Kelkar Library, IIT Kanpur (5)
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- PK Kelkar Library, IIT Kanpur (5)
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- Reference (1)
- Technical Report (5)
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- National Aeronautics and Space Administration ( NASA ) (1)
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- Spacecraft (1)

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	1.	Low-speed test of an all-flexible parawing landing a lifting-body spacecraft [ NASA TN D-4010 ] by Bugg, Frank M \| Sleeman, William C. Material type: Book; Format: print ; Literary form: not fiction Description: 32p.Publisher: Washington, D.C. Nasa 1967Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4010] (1). Add to cart (remove)
	2.	WIND-TUNNEL STUDIES OF EFFECTS OF CONSTRUCTION METHODS, DESIGN DETAILS, AND CANOPY SLOTS ON THE AERODYNAMIC CHARACTERISTICS OF SMALL-SCALE ALL-FLEXIBLE PARAWINGS by Fournier,Paul G \| Sleeman,William C. Material type: Book Description: 91.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5974] (1). Add to cart (remove)
	3.	LOW-SPEED LONGITUDINAL CHARACTERISTICS OF AN AIRPLANE CONFIGURATION INCLUDING EFFECTS OF CANARD AND WING TRAILING-EDGE FLAP CONTROLS IN COMBINATION by Spencer,Bernard \| Sleeman,William C. Material type: Book Description: 50.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA MEMO 4-22-59L] (1). Add to cart (remove)
	4.	THE ROLLING MOMENT DUE TO SIDESLIP OF SWEPT WINGS AT SUBSONIC AND TRANSONIC SPEEDS by Polhamus,Edward C \| Sleeman,William C. Material type: Book Description: 81.Publisher: Nasa, Washington, D.C. 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-209] (1). Add to cart (remove)
	5.	INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE USE OF LOW AUXILIARY TAIL SURFACES HAVING DIHEDRAL TO IMPROVE THE LONGITUDINAL AND DIRECTIONAL STABILITY OF A T-TAIL MODEL AT HIGH LIFT by Sleeman,William C. Material type: Book Description: 23.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-804] (1). Add to cart (remove)

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