Normal view MARC view ISBD view

FLIGHT EVALUATION OF THREE TECHNIQUES OF DEMONSTRATING THE MINIMUM FLYING SPEED OF A DELTA-WING AIRPLANE

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1964Description: 29.DDC classification: NASA | TN D-2337

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-2337 (Browse shelf)	Not for loan		TR13617

Total holds: 0

Previous								Next
Previous	NASA TN D-2334 EFFECTS OF DISTRIBUTED ROUGHNESS HEIGHT ON AERODYNAMIC CHARACTERISTICS AND BOUNDARY -LAYER TRANSITION OF A WING-BODY-TALL CONFIGURATION AT A MACH NUMBER OF 1.61	NASA TN D-2335 EFFECT OF STAGE SPACING ON PERFORMANCE OF 3.75-INCH-MEAN-DIAMETER TWO-STAGE TURBINE HAVING PARTIAL ADMISSION IN THE FIRST STAGE	NASA TN D-2336 PRELIMINARY ANALYSIS OF VARIATION OF PITCH MOTION OF A VEHICLE IN A SPACE ENVIRONMENT DUE TO FUEL SLOSHING IN A RECTANGULAR TANK	NASA TN D-2337 FLIGHT EVALUATION OF THREE TECHNIQUES OF DEMONSTRATING THE MINIMUM FLYING SPEED OF A DELTA-WING AIRPLANE	NASA TN D-2338 A SIMPLE ABORT SCHEME FOR LUNAR LANDINGS	NASA TN D-2339 CORRELATION GRAPHS FOR SUPERSONIC FLOW AROUND RIGHT CIRCULAR CONES AT ZERO YAW IN AIR AS A PERFECT GAS	NASA TN D-2340 HEAT-TRANSFER MEASUREMENTS ON A FLAT PLATE AND ATTACHED FINS AT MACH NUMBERS OF 3.51 AND 4.44	Next

Bound With Nasa Tn D-2331-2336,2338-2340

There are no comments for this item.

PKK Library