Simulation of flight test conditions in the langley pilot transonic cryogenic tunnel [NASA TN D 7811-7820 (Record no. 561386)
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| fixed length control field | 03278nam a22001817a 4500 |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20200219112202.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 200219b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE | |
| Transcribing agency | IIT Kanpur |
| 041 ## - LANGUAGE CODE | |
| Language code of text/sound track or separate title | eng |
| 110 ## - MAIN ENTRY--CORPORATE NAME | |
| Corporate name or jurisdiction name as entry element | NASA : National Aeronautics and Space Administration |
| 245 ## - TITLE STATEMENT | |
| Title | Simulation of flight test conditions in the langley pilot transonic cryogenic tunnel [NASA TN D 7811-7820 |
| Statement of responsibility, etc | Kilgore, Robert A. [...et al.] |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) | |
| Place of publication | Washington |
| Name of publisher | NASA |
| Year of publication | 1974 |
| 300 ## - PHYSICAL DESCRIPTION | |
| Number of Pages | various pagings |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE | |
| Title | National Aeronautics and Space Administration, NASA Technical Report |
| 505 ## - FORMATTED CONTENTS NOTE | |
| Formatted contents note | NASA TN D-7812 : Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities; NASA TN D-7813 : Calculation of the twist distribution of wings designed for cruise at transonic speeds; NASA TN D-7814 : The effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration; NASA TN D-7815 : Experimental investigation of the cornering characteristics of 18*5.5, type VII, aircraft tires with different tread patterns; NASA TN D-7816 : Static tests of a simulated upper surface blown jet-flap configuration utilizing a full-size turbofan engine; NASA TN D-7817 : Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model; NASA TN D-7818 : Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades; NASA TN D-7819 : Flight-determined lag of angle-of-attack and angle-of-sideslip sensors in the YF-12A airplane from analysis of dynamic maneuvers; NASA TN D-7820 : Digital program for solving the linear stochastic optimal control and estimation problem; |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical Term | NASA Technical Report |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | Books |
| Withdrawn status | Lost status | Damaged status | Not for loan | Collection code | Permanent Location | Current Location | Date acquired | Accession Number | Koha item type |
|---|---|---|---|---|---|---|---|---|---|
| COMPACT STORAGE (BASEMENT) | PK Kelkar Library, IIT Kanpur | PK Kelkar Library, IIT Kanpur | 2020-02-19 | TR002549 [TN D7811-D | Technical Report |