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EXPERIMENTAL INVESTIGATION OF BLAST LOADING ON AN AIRFOIL IN MACH 0.7 AIRFLOW WITH INITIAL ANGLE-OF-ATTACK CHANGE OF 28 (DEGRE)

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BookPublisher: Nasa, Washington, D.C. 1965Description: 25.DDC classification: NASA | TN D-2876

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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-2876 (Browse shelf)	Not for loan Untraceable		TR13459

Total holds: 0

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Previous	NASA TN D-2873 SEEDING CRITERION FOR NONEQUILIBRIUM MAGNETOHYDRODYNAMIC GENERATORS	NASA TN D-2874 A COMPUTER PROGRAM TO CALCULATE ARTIFICIAL RADIATION BELT DECAY FACTORS	NASA TN D-2875 OBSERVATIONS ON AFFINITY AND KINETIC BEHAVIOR OF SOME CHEMICAL REACTIONS	NASA TN D-2876 EXPERIMENTAL INVESTIGATION OF BLAST LOADING ON AN AIRFOIL IN MACH 0.7 AIRFLOW WITH INITIAL ANGLE-OF-ATTACK CHANGE OF 28 (DEGRE)	NASA TN D-2877 SOME NONASYMPTOTIC EFFECTS ON THE SONIC BOOM OF LARGE AIRPLANES	NASA TN D-2878 FEASIBILITY STUDY OF HIGH-TEMPERATURE SYNTHETIC-AIR HEATER FOR USE WITH A MACH 8 TO 9 HYPERSONIC TUNNEL	NASA TN D-2879 DESIGN AND OVERALL PERFORMANCE OF A TWO-STAGE AXIAL-FLOW PUMP WITH A TANDEM-ROW INLET STAGE	Next

Bound With Nasa Tn D-2871-2875,2877-2880

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