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A NEW TECHNIQUE FOR CALCULATING REENTRY BASE HEATING.

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BookPublisher: Nasa, Washington, D.C. 1973Description: 38.DDC classification: NASA | TN D-7508

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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-7508 (Browse shelf)	Not for loan		TR11587

Total holds: 0

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Previous	NASA TN D7505 EFFECT OF CANARD LOCATION AND AERODYNAMIC-CENTER SHIPTS RELATED TO MANEUVERING AIRCRAFT AT TRANSONIC SPEEDS.	NASA TN D-7506 PRESSURE MEASUREMENTS ON THE LEADING EDGE OF A SWEFT WING AT MATCH 2.2	NASA TN D-7507 ENGINEERING PREDICATION OF TURBULENT SKIN FRICTION AND HEAT TRANSFER IN HIGH-SPEED FLOW.	NASA TN D-7508 A NEW TECHNIQUE FOR CALCULATING REENTRY BASE HEATING.	NASA TN D-7509 EN ROUTE POSITION AND TIME CONTROL OF AIRCRAFT USING KALAMAN FILTERING OF RADIO AID DATA.	NASA TN D-7510 COMPARISON OF MEASURED AND CALCULATED VELOCITY PROFILES OF A LAMINAR INCOMPRESSIBLE FREE JET AT LOW REYNOLDS NUMBERS.	NASA TN D-7513 - FILM COOLING IN A COMBUSTOR OPERATING AT FUEL-RICH EXIT CONDITIONS	Next

Bound With Nasa Tn D 7500-7507,7509-10.Lack No-7503.

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