Normal view MARC view ISBD view

EXPERIMENTAL INVESTIGATION OF THE EFFECTS OF MACH NUMBER, STABILIZER DIHEDRAL, AND FIN TORSIONAL STIFFNESS ON THE TRANSONIC FLUTTER CHARACTERISTICS OF A TEE-TAIL

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1961Description: 24.DDC classification: NASA | TN D-924 -

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-924 - (Browse shelf)	Not for loan		TR10310

Total holds: 0

Previous								Next
Previous	NASA TN D-92 MEASURED AND THEORETICAL FLOW FIELDS BEHIND A RETANGULAR AND A TRIANGULAR WING UP TO HIGH ANGLES OF AATACK AT A MACH NUMBER OF 2.46.	NASA TN D-922 - REPEATABILITY, DRIFT, AND AFTEREFFECT OF THREE TYPES OF AIRCRAFT ALTIMETERS	NASA TN D-923 - AUTOMATIC TERMINAL GUIDANCE SYSTEM FOR RENDEZVOUS WITH A SATELLITE	NASA TN D-924 - EXPERIMENTAL INVESTIGATION OF THE EFFECTS OF MACH NUMBER, STABILIZER DIHEDRAL, AND FIN TORSIONAL STIFFNESS ON THE TRANSONIC FLUTTER CHARACTERISTICS OF A TEE-TAIL	NASA TN D-925 - MEASUREMENTS AND CALCULATIONS OF THE EFFECTS OF DISTORTIONS IN THE COLLECTOR SURFACE ON EFFICIENCIES OF UMBRELLA-TYPE SOLAR COLLECTORS	NASA TN D-926 - AERODYNAMIC CHARACTERISTICS OF LOW-ASPECT-RATIO WINGS IN CLOSE PROXIMITY TO THE GROUND	NASA TN D-927 - FREE-FLIGHT INVESTIGATION OF RADIO-CONTROLLED MODELS WITH PARAWINGS	Next

Bound With Nasa Tn D-921-30

There are no comments for this item.

PKK Library