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STATIC LIFT, DRAGE, AND PITCHING-MOMENT CHARACTERISTICS OF WINGS WITH ARROW AND MODIFIED-DIMOND PLAN FORMS COMBINED WITH SEVERAL DIFFERENT BODIES AT MACH NUMBERS OF 2.97, 3.35, AND 3.71

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BookPublisher: Nasa, Washington, D.C. 1959Description: 50.DDC classification: NASA | MEMO 1-24-59L

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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 1-24-59L (Browse shelf)	Not for loan		TR17738

Total holds: 0

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Previous	NASA MEMO 1-23-59L MAXIMUM MEAN LIFT COEFFICIENT CHARACTERISTICS AT LOW TIP MACH NUMBERS OF A HOVERING HELICOPTER ROTOR HAVING AN NACA 64 A012 AIRFOIL SECTION	NASA MEMO 12-4-58L - PRELIMINARY MEASUREMENT OF THE THE NOISE CHARACTERISTICS OF SOME JET-AUGMENTED CONFIGURATIONS	NASA MEMO 12-4-58W HEAT TRANSFER IN THE TURBULENT INCOMPRESSIBLE BOUNDRY LAYER IV- EFFECT OF LOCATION OF TRANSITION AND PREDICTION OF HEAT TRANSFER IN A KNOWN TRANSITION REGION.	NASA MEMO 1-24-59L STATIC LIFT, DRAGE, AND PITCHING-MOMENT CHARACTERISTICS OF WINGS WITH ARROW AND MODIFIED-DIMOND PLAN FORMS COMBINED WITH SEVERAL DIFFERENT BODIES AT MACH NUMBERS OF 2.97, 3.35, AND 3.71	NASA MEMO 12-5-58W INTERACTION EFFECTS PRODUCED BY JET EXHAUSTING LATERALLY NEAR BASE OF OGIVE-CYLINDER MODEL IN SUPERSONIC MAIN STREAM.	NASA MEMO 1-25-59L EFFECT OF CONVEX LONGITUDINAL CURVATURE ON THE PLANING CHARACTERISTICS OF A SURFACE WITHOUT DEAD RISE	NASA MEMO 1-26-59L FLIGHT INVESTIGATION OF THE SURFACE PRESSURE DISTRIBUTION AND FLOW FIELD AROUND AN ELLIPTICAL SPINNER	Next

Bound With Nasa Memo 1-15-59l-23,25-31, Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l

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