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COMPARISON OF FLIGHT PRESSURE MEASUREMENTS WITH WIND-TUNNEL DATA AND THEORY FOR THE FORWARD FUSELAGE OF THE X-15 AIRPLANE AT MACH NUMBERS FROM 0.8 TO 6.0

By: Pyle,Jon S.
Material type: materialTypeLabelBookPublisher: Nasa, Washington, D.C. 1964Description: 29.DDC classification: NASA | TN D-2241
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Item type Current location Collection Call number Status Date due Barcode Item holds
Technical Report Technical Report PK Kelkar Library, IIT Kanpur
General Stacks NASA TN D-2241 (Browse shelf) Not for loan 65612
Total holds: 0

Bound With Nasa Tn D-2242-2250

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