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AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE UNSWEPT WING-BODY-TALL CONFIGURATION WITH BLOWING APPLIED OVER THE FLAP AND WING LEADING EDGES.

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BookPublisher: Nasa, Washington, D.C. 1960Description: 213.DDC classification: NASA | TN D-407

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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 TN D-407 (Browse shelf)	Not for loan		TR15962

Total holds: 0

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Previous	NASA TN D-405 INVSTIGATION OF TANDEM-WHEEL AND AIR-JET ARRANGMENTS FOR IMPROVEING BRAKING FRICTION ON WHET SURFACES.	NASA TN D-4050 PERFORMANCE OF X 258 THIRD-STAGE MOTOR ON DELTA 36 (OT-3)	NASA TN D-406 EFFECTS OF AIR CONTAMINATION IN A HELIUM TUNNEL.	NASA TN D-407 AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE UNSWEPT WING-BODY-TALL CONFIGURATION WITH BLOWING APPLIED OVER THE FLAP AND WING LEADING EDGES.	NASA TN D-4076 STATIC STABILITY CHARACTERISTICS AT MACH NUMBERS FROM 1.90 TO 4.63 OF A 76 DEGREE SWEPT ARROW WING MODEL WITH VARIATIONS IN HORIZONTAL-TAIL HEIGHT WING HEIGHT, AND DIHEDRAL	NASA TN D-408 THE BLUNT PLATE IN HYPERSONIC FLOW.	NASA TN D-4092 AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE V/ STOL TRANSPORT MODEL WITH LIFT AND LIFT-CRUISE FANS.	Next

Bound With Nasa Tn D-401-406,408-410.Lack No-402.

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