Normal view MARC view ISBD view

WIND-TUNNEL INVESTIGATION AT A MACH NUMBER OF 2.01 OF THE SONIC-BOOM CHARACTERISTICS OF THREE WIND-BODY COMBINATIONS DIFFERING IN WING LONGITUDINAL LACATION

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1962Description: 17.DDC classification: NASA | TN D-1384 -

average rating: 0.0 (0 votes)

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-1384 - (Browse shelf)	Not for loan		TR9552

Total holds: 0

Previous								Next
Previous	NASA TN D-1380 EFFECTS OF ANGLE OF ATTACK AND THICKNESS RATIO ON THE FLUTTER OF RIGID UNSWEPT DIAMOND-AIRFOIL-SECTION WING AT A MACH NUMBER OF 10.0	NASA TN D-1382 - SLIPSTREAM FLOW AROUND SEVERAL TILT-WING VTOL AIRCRAFT MODELS OPERATING NEAR THE GROUND	NASA TN D-1383 - RADIATION EXPOSURE IN SUPERSONIC TRANSPORTS	NASA TN D-1384 - WIND-TUNNEL INVESTIGATION AT A MACH NUMBER OF 2.01 OF THE SONIC-BOOM CHARACTERISTICS OF THREE WIND-BODY COMBINATIONS DIFFERING IN WING LONGITUDINAL LACATION	NASA TN D-1385 - PANEL FLUTTER TESTS ON FULL-SCALE X-15 LOWER VERTICAL STABILIZER AT MACH NUMBER OF 3.0	NASA TN D-1386 - EXPERIMENTAL INVESTIGATION OF THE EFFECTS OF COMPRESSIVE STRESS ON THE FLUTTER OF A CURVED PANEL AND A FLAT PANEL AT SUPERSONIC MACH NUMBERS	NASA TN D-1387 - ATMOSPHERE AS A PART OF THE SPACE ENVIRONMENT	Next

Bound With Nasa Tn D-1381-90

There are no comments for this item.

PKK Library