PKK Library catalog › Results of search for 'au:"Lichtenstein,Jacob H"'

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	1.	SOME STATIC, OSCILLATORY, AND FREE-BODY TESTS OF BLUNT BODIES AT LOW SUBSONIC SPEEDS by Lichtenstein,Jacob H. Material type: Book Description: 30.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA MEMO 2-22-59L -] (1). Add to cart (remove)
	2.	NASA Technical Note [NASA TN D-6113]: A statistical study of ability of simulated pilots to control the approach and descent of the lunar module to the lunar surface by Washington. National Aeronautics and Space Administration (NASA) \| Lichtenstein, Jacob H. Material type: Book Description: 57p.Publisher: Washington NASA 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1). Add to cart (remove)
	3.	A PRELIMINARY INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE ON THE ROLLING DERIVATIVES OF AN UNSWEPT-WING MODEL OSCILLATING IN ROLL by Fisher,Lewis R,Lichtenstein,Jacob H \| Williams,Katherine D. Material type: Book Description: 29.Publisher: Naca, Washington 1955Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NACA TN 3554] (1). Add to cart (remove)
	4.	COMPUTED LATERAL POWER SPECTRAL DENSITY RESPONSE OF CONVENTIONAL AND STOL AIRPLANES TO RANDOM ATMOSPHERIC TURBULENCE by Lichtenstein,Jacob H. Material type: Book Description: 88.Publisher: Nasa, Washington, D.C. 1974Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-7444] (1). Add to cart (remove)
	5.	LOW-SPEED INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE OF OSCILLATION IN SIDESLIP ON THE LATERAL STABILITY DERIVATIVES OF A 60(DEGREE) DELTA WING, A 45(DEGRE) SWEPTBACK WING, AND AN - - - by Lichtenstein,Jacob H \| Williams,James L. Material type: Book Description: 19.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-896] (1). Add to cart (remove)

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