Search

Advanced search

Normal view MARC view ISBD view

A method of determining aerodynamic- influence coefficients from wind-tunnel data for wings at supersonic speeds [NASA TN D-801--TN D-810]

By: Gainer,Patrick A.

Publisher: Nasa Washington, D.C. 1961Description: 34p.

average rating: 0.0 (0 votes)

Holdings ( 1 )
Title notes
Comments ( 0 )

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-801 (Browse shelf)	Not for loan		65481

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser

Previous								Next
Previous	NASA TN D-779 FLIGHT INVESTIGATION USING VARIABLE-STABLITY AIRPLANES OF MINIMUM STABILITY REQUIREMENTS FOR HIGH-SPEED, HIGH-ALTITUDE VEHICLES	NASA TN D-780 A METHODS FOR OBTAINING THE NONLINEAR AERODYNAMIC STABILITY CHARACTERISTICS OF BODIES OF REVOLUTION FROM FREE-FLIGHT TESTS	NASA TN D-792 - ATTITUDE CONTROL REQIREMENTS FOR HOVERING DETERMINED THROUGH THE USE OF A PILOTED FLIGHT SIMULATOR	NASA TN D-801 A method of determining aerodynamic- influence coefficients from wind-tunnel data for wings at supersonic speeds [NASA TN D-801--TN D-810]	NASA TN D-802 A PRELIMINARY INVESTIGATION OF THE EFFECT OF BUMPERS AS A MEANS OF REDUCING PROJECTILE PENETRATION	NASA TN D-803 EFFECTS OF MASS-LOADING VARIATIONS AND APPLIED MOMENTS ON MOTION AND CONTROL OF A MANNED ROTATING SPACE VEHICLE	NASA TN D-804 INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE USE OF LOW AUXILIARY TAIL SURFACES HAVING DIHEDRAL TO IMPROVE THE LONGITUDINAL AND DIRECTIONAL STABILITY OF A T-TAIL MODEL AT HIGH LIFT	Next

Bound With Nasa TN D-802 to TN D-810 [Accession Nos : TR015836 to 015844]

There are no comments for this item.

Log in to your account to post a comment.

Powered by Koha