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AN INTEGRATED APPROACH TO THE ANALYSIS AND DESIGN OF WINGS AND WING-BODY COMBINATIONS IN SUPERSONIC FLOW

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BookPublisher: Nasa, Washington, D.C. 1966Description: 13.DDC classification: NASA | TN D-3685

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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-3685 (Browse shelf)	Not for loan		TR16112

Total holds: 0

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Previous	NASA TN D-3682 EXPERIMENTAL STUDY OF EFFECTS OF ELECTRON IRRADIATION FROM 20 KEV TO 1 MEV ON A POLYETHYLENE TEREPHTHALATE CAPACITOR-TYPE METEOROID DETECTOR	NASA TN D-3683 LIMITATIONS ON INERTIAL SENSOR TESTING PRODUCED BY TEST PLATFORM VIBRATIONS	NASA TN D-3684 NONSTEADY LIQUID AND GAS FLOW WITH HEAT ADDITION AND SHOCK PERTURBATIONS	NASA TN D-3685 AN INTEGRATED APPROACH TO THE ANALYSIS AND DESIGN OF WINGS AND WING-BODY COMBINATIONS IN SUPERSONIC FLOW	NASA TN D-3686 DEVELOPMENT OF SENSORS TO OBTAIN IN-FLIGHT ABLATION MEASUREMENTS OF THERMAL-PROTECTION MATERIALS	NASA TN D-3687 COMPARISON OF RESULTS OF TWO SIMULATIONS EMPLOYING FULL-SIZE VISUAL CUES FOR PILOT-CONTROLLED GEMINI-AGENA DOCKING	NASA TN D-3688 A FULL-SIZE PILOT-CONTROLLED DOCKING SIMULATION OF THE APOLLO COMMAND AND SERVICE MODULE WITH THE LUNAR MODULE	Next

Bound With Nasa Tn D-3681-3684,3686-3690

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