Normal view MARC view ISBD view

MODIFIED MATRIX METHOD FOR CALCULATING STEADY-STATE SPAN LODING ON FLEXIBLE WINGS IN SUBSONIC FLIGHT

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1959DDC classification: NASA | MEMO 5-26-59L

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 MEMO 5-26-59L (Browse shelf)	Not for loan Untraceable		TR7411

Total holds: 0

Previous								Next
Previous	NASA MEMO 5-24-59L A SIMPLE METHOD FOR DETERMINING HEAT TRANSFER, SKIN FRICTION, AND BOUNDARY-LAYER THICKNESS FOR HYPERSONIC LAMINAR BOUNDARY-LAYER FLOWS IN A PRESSURE GRADIENT	NASA MEMO 5-25-59 - 1958 NASA/USAF SPACE PRIBES (ABLE-1)	NASA MEMO 5-25-59L INVESTIGATION OF THE STABILITY OF VERY FLAT SPIN AND ANALYSIS OF EFFECTS OF APPLYING VARIOUS MOMENTS UTILIZING THE THREE MOMENT EQUATIONS OF MOTION	NASA MEMO 5-26-59L MODIFIED MATRIX METHOD FOR CALCULATING STEADY-STATE SPAN LODING ON FLEXIBLE WINGS IN SUBSONIC FLIGHT	NASA MEMO 5-28-59L INVESTIGATION ON THE USE OF A FREELY ROTATING ROTOR AT THE COWL FACE OF A SUPERSONIC CONICAL INLET TO REDUCE INLET FLOW DISTORTION	NASA MEMO 6-10-59L - EXPERIMENTAL INVESTIGATION OF THE HEAT-TRANSFER RATE TO A SERIES OF 20(DEGREE) CONES OF VARIOUS SURFACE FINISHES AT A MACH NUMBER OF 4.95	NASA MEMO 6-11-59L - LOW-SPEED INVES. OF THE EFFECTS OF HORIZONTAL-TAIL AREA & WING SWEEP ON THE STATIC LONGITUDINAL STABILITY & CONTROL CHARS. OF AN AIRPLANE CONFIGURATION HAVING TAIL SURFACES OUTBOARD OF THE WING TIPS	Next

Bound With Nasa Memo 5-12-59l-5-25-59l And 5-28-59l Lack No.14-17, 19, 21-22, 27

There are no comments for this item.

PKK Library