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Measurement of aerodynamic forces on hypersonic models in an impulse facility using an accelerometer balance (R)

Abhinav Kumar, K.S.N.

Measurement of aerodynamic forces on hypersonic models in an impulse facility using an accelerometer balance (R) - - Mumbai IIT 2009 - 40 p. 30 cm - .

ISBN:

Subjects--Topical Terms:
Menezes, V.
Theses and Dissertations
Aerodynamic load , Hypersonic , Accelerometers , Shock tunnel

Universal Decimal Class. No.: 043:629.136.2:533.6.01Abh

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